university of hawai'l library
TRANSCRIPT
UNIVERSITY OF HAWAI'l LIBRARY
THE INFLUENCE OF ELECTRON DEGENERACYON THE MSW EFFECT IN THE SUN
A THESIS SUBMITTED TO THE GRADUATE DIVISION OFTHE UNIVERSITY OF HAWAI'I
IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FORTHE DEGREE OF
MASTER OF SCIENCE
IN
PHYSICS
May 2004
by
Christopher Wrenn
Thesis Committee:
John G. Learned, ChairpersonMichael W. Peters
Sandip Pakvasa
Acknowledgements
I would like to express appreciation to Dr. John Learned for giving me theintellectual freedom to search the cosmos to find of a suitable thesis topic and inassisting me to identify research-worthy subject matter.
I am indebted to Dr. Michael Peters for suggesting various approaches tothe problems raised and for insisting that the solutions offered be asincontrovertible as time allows.
I am sincerely grateful to Dr. Sandip Pakvasa for his unbendingconsideration in taking care that my thesis topic be both interesting and original.
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Table of Contents
Abstract viList of Abbreviations viiList of Tables viiiList of Figures .ixIntroduction 11.0 The Theory of Partial Degeneracy 32.0 The MSW Effect 14
2.1 The Interaction Hamiltonian 172.2 Two Neutrino Vacuum Oscillations 222.3 Neutrino Flavor Conversion in Matter 292.4 Neutrino Propagation Equation in Matter. 322.5 Propagation Equations for Homogeneous Densities 362.6 Neutrino Flavor Conversion in Media with
Nonhomogeneous Densities: The MSW Effect 383.0 Partial Electron Degeneracy in the Sun 544.0 Neutrino-Emitting Thermonuclear Reactions 59
4.1 Nuclear Reaction Rates 644.2 Cross Sections for Non-Resonant Reactions 70
5.0 Standard Solar Models 735.1 Equations of Stellar Structure and Evolution 745.2 Numerical Methods for Solar Modeling 805.3 Standard Solar Models 82
6.0 Solar Neutrinos and Neutrino Experiments 886.1 Solar Neutrino Experiments 926.2 Experimental Findings and Upcoming Studies 96
7.0 The Influence of Electron Degeneracy on the MSW Effect. 1007.1 Analytic Solutions of the MSW Effect in the Sun 1017.2 Numerical Calculations of Ve Evolutionary Profiles 108
8.0 Conclusion and Future Prospects 1158.1 Neutrinos and Cosmology 1178.2 Neutrinos and Stellar Physics 1238.3 Neutrinos and Degenerate Electrons 126
Appendix A: Fierz transformation of the interaction Hamiltonian 130Appendix B: Derivation of the energy rate formula 133Appendix C: Solution of the neutrino eigenvalue problem 138Appendix D: Tranform of the neutrino vacuum propagation equation 139Appendix E: Tranform of the neutrino matter propagation equation 141Figures 143References 196
v
ABSTRACT
The relatively high densities in the interior of the Sun cause a small fraction of the
electrons there to exist in a degenerate state. Because this region of electron
degeneracy overlaps with the same location where the MSW effect is known to
occur, a study was made to quantify the influence that degenerate electrons have
on the electron neutrino survival probability of neutrinos exiting the solar surface.
Three different numerical methods were used to determine the influence that the
Sun's degenerate electrons have on the on the MSW effect - where varying
electron density profiles allow neutrinos to change flavor as they pass through
stellar interiors. Analytic and numerical solutions showed no observable
variations in the electron neutrino survival probabilities whether or not degenerate
electrons were included in the solar density profiles.
VI
LIST OF ABBREVIATIONS
AU = Astronomical UnitBooNE = Booster Neutrino ExperimentCNO = Carbon-Nitrogen-OxygenCKM = Cabibbo-Kobayashi-MaskawaCP = Charge-ParityCPT = Charge-Parity-TimeEOS = Equation of StateFD = Fermi-DiracGNO = Gallium Neutrino ObservatoryGONG = Global Oscillation Network GroupGRB = Gamma-Ray BursterGSW = Glashow, Salam and WeinbergKG = Klein-GordonKamLAND = Kamioka Liquid Scintillator Anti-Neutrino DetectorKATRIN = Karlsruhe Tritium Neutrino ExperimentLMA = Large Mixing AngleLSND = Liquid Scintillator Neutrino DetectorLZS = Landau, Zener and SttickelbergMB = Maxwell-BoltzmannMNS = Maki, Nakagawa and SakataMSW = Mikheyev, Smirnov and WolfensteinSAGE = Soviet-American Gallium ExperimentSK = Super-KamiokandeSM = Standard ModelSN = SupernovaSNO = Sudbury Neutrino ObservatorySNU = Solar Neutrino Unit (10-36 v captures/target atom/s)SORO = Solar and Reliospheric ObservatorySSM = Standard Solar ModelSU(5) = Special Unitary Group (n =5)V-A = Vector minus AxialWI = Weak InteractionWMAP = Wilkinson Microwave Anisotropy ProbeZAMS = Zero Age Main Sequence
vii
Table 1:Table 2:Table 3:Table 4:Table 5:Table 6:Table 7:Table 8:
Table 9:Table 10:
LIST OF TABLES
Nuclear reaction data for pp1 branchNuclear reaction data for pp2 branchNuclear reaction data for pp3 branchNuclear reaction data for the carbon cycleReaction data for neutrino processesElectron-electron neutrino cross-sectionsCalculated neutrino fluxesAnalytic and Numerical Results of P(ve ---7 v.)
Neutrino propertiesSolar parameters
Vlll
Figure 1:Figure 2:Figure 3:Figure 4:Figure 5:Figure 6:Figure 7:Figure 8:Figure 9:Figure 10:Figure 11:Figure 12:Figure 13:Figure 14:Figure 15:Figure 16:Figure 17:Figure 18:Figure 19:Figure 20:Figure 21:Figure 22:Figure 23:Figure 24:Figure 25:Figure 26:Figure 27:Figure 28:Figure 29:Figure 30:Figure 31:Figure 32:Figure 33:Figure 34:Figure 35:Figure 36:
Figure 37:
Figure 38:
Figure 39:
LIST OF FIGURES
Partial, Complete and Maxwell-Boltzmann DistributionsFermi distribution function versus energyNeutrino level crossing diagramFeynman diagrams of electron-neutrino scatteringMSW trianglePartial electron degeneracy in the solar core (Stix)Electron number density difference with and without degeneracySolar density profile (BP2000)Partial electron degeneracy in the solar coreSolar density profile (JCDI987)Comparison of density profiles for two SSMsThe log of electron density versus solar radius (BP2000)Gamow peak (theoretical)Gamow peak (experimental)Log of electron density versus solar radius (sterile neutrinos)Solar neutrino flux (Balantekin)Neutrino production as a function of radiusCalculated neutrino spectraTemperature dependence on solar neutrino fluxesLevel crossing in the case of SN neutrinosPre-SN density profileEvolution of neutrinos with different energiesSurvival probabilitiesProfile of survival probabilitiesLevel crossingMSW contour plotElectron number density vs. solar radius (JCDI987)Electron number density vs. solar radius (BP2000)Electron number densities for BP2000 and JCD1987Induced mass A vs. sin2 28M showing resonance
.Induced mass A vs. sin2 28M using LMA parametersNeutrino level crossing diagram using LMA parametersSolar pp chainDegenerate density vs. exponential density profileDegenerate vs. nondegenerate exponential profilesEvolution of P(ve --7 ve ) using incorrect mixing matrix
Evolution of P(ve --7 ve ) using corrected mixing matrix
Evolution of P(ve --7 ve ) using JCD SSM (Degenerate) step=1
Evolution of P(ve --7 v e ) using JCD SSM (Nondegenerate)
ix
Figure 40:
Figure 41:
Figure 42:
Figure 43:
Figure 44:Figure 45:Figure 46:Figure 47:Figure 48:Figure 49:
Figure 50:
Figure 51:
Figure 52:
Figure 53:
Figure 54:
Percent difference in P(ve ~ vJ (Degenerate-Nondegenerate)
Evolution of P(ve ~ ve> using JCD SSM (Degenerate) step=1/2
Evolution of P(ve ~ ve ) using JCD SSM (Nondegenerate)
Percent difference in P(ve ~ ve> (Degenerate-Nondegenerate)
Probability evolution as a function of energy (Ev = 14 MeV)Probability evolution as a function of energy (By = 6 MeV)Probability evolution as a function of energy (Ev = 2 MeV)Probability evolution as a function of energy (Ev = 0.86 MeV)Interpolated ratio of FD integralsEvolution of P(ve ~ ve> using BP SSM (Degenerate) step=1
Evolution of P(ve ~ v e ) using BP SSM (Nondegenerate)
Percent difference in P(ve ~ ve> (Degenerate-Nondegenerate)
Evolution of P(ve ~ ve> using BP SSM (Nondegenerate) 8 = 33°
Evolution of P(ve ~ ve ) using BP SSM (Degenerate) 8 = 33°
Percent difference in P(ve ~ vJ (Degenerate-Nondegenerate)
x
Introduction
As a source of neutrinos of various fluxes and energies, the Sun offers us
an excellent astrophysical system for studying the low energy regime of particle
physics. The goal of this work is to theoretically determine the effect of
degenerate electrons in the solar core on the flavor transformation of neutrinos via
electron-electron neutrino scattering processes, i.e., vee- -7 e-va . Derivations and
details of the relevant physics will describe 1) partial degeneracy, 2) the MSW
effect, 3) partial degeneracy in the Sun, 4) neutrino-creating thermonuclear
reactions, 5) equations of stellar structure, evolution and solar modeling, as well
as 6) recent findings from neutrino experiments on the nature of solar neutrinos.
Section 7 contains the numerical calculations of the influence of degenerate
electrons on electron neutrinos passing through the Sun. This work concludes
with a number of important cosmological and stellar issues associated with
neutrinos, in addition to the relationship between neutrinos and degenerate
electrons in supernovae and the Sun.
The anti-neutrino detecting facility at KamLAND has obtained compelling
evidence that the MSW effect is the leading solution to the solar neutrino problem.
The MSW effect, named after its founders Mikheyev, Srnirnov and Wolfenstein,
describes a quantum mechanical effect whereby a fraction of the electron
1
neutrinos created in thermonuclear processes in the solar core are transformed
into other flavors as they pass through a region of critical solar electron density.
From such low energy studies of the neutrinos emerging from the Sun (and
supernovae), detailed studies can be made into the nature of the standard
electroweak model of physics. It is conceivable that such studies may lead to a
quantifiable determination of the masses of the various families of neutrinos with
potentially profound consequences for the Standard Model, supernova physics
and cosmology. The most sought after parameters in neutrino physics today are
their absolute masses. 1
Some investigators have considered the possibility that the MSW effect
may help revive stalled supernova (SN) explosions - known as the supernova
problem -- through neutrino heating processes [2, 3]. Extremely strong magnetic
fields (_10160) have also been identified as potentially critical for re-igniting the
stagnated supernova shock wave [4]. Because of the long waiting period between
Type II galactic supernovae, other researchers have suggested measuring pre-
supernova neutrinos from nearby stars in advanced burning stages [5]. Thus,
there remain a significant number of undetermined properties of neutrinos and
outstanding unresolved astrophysical matters to keep neutrino researchers and
astrophysicists busy for some time.
1 While neutrinos are assumed to be massless in standard SU(2)XU(1) electroweak theories,neutrinos with nonzero masses arise naturally in a number of grand unified theories, such asSO(lO)[l].
2
1.0 The Theory of Partial Degeneracy
In atoms and molecules, the Slater determinant (constructed from
electron spin-orbitals) ensures that the wave function describing a system of spin-
'h particles will be totally antisymmetric under particle interchange. The Slater
determinant is a mathematical statement of the Pauli exclusion principle which
states that no two fermions can have the same spatial and spin quantum numbers;
in other words, no two fermions can exist in precisely the same quantum state of
motion. Because of high temperatures and pressures in the interior of the Sun, the
atoms there are completely ionized. So, instead of describing the particles in the
solar interior in terms of spin-orbitals, they can more accurately be represented as
a neutral system of non-interacting free electrons and nuclei. In what follows, the
electronic component of the solar plasma will be of primary interest.
Pauli's principle for free electrons states that only two electrons with
oppositely directed spins can occupy a region of momentum space whose unit cell
volume is h3 where h is Planck's constant. According to Fermi's theory of a free
electron gas [6], completely degenerate electrons must distribute themselves in
such a way as to form the lowest possible energy state at the absolute zero of
temperature. The maximum possible energy that such a completely degenerate
(i.e., T = 0 K) system can have is Cf =~ (3lZ'2 ne t 3where ne is the electron
2me
number density equal to the number of electrons per unit volume, Ii is the Planck
3
constant divided by 2n, me is the electron mass, and Cf is the Fermi energy for the
system. At the absolute zero of temperature (when the matter has radiated its
energy away), the state that exists is the only possible configuration left [7], i.e.,
the lowest possible energy state. There are many assumptions in this rich theory
of degeneracy besides those of a neutral, non-interacting gas of free nuclei and
electrons. For instance, it should be kept in mind that, as a species of Gibbsian
statistics, the assumptions of a priori probability distributions, and the use of
Stirling's approximation (needed to obtain the most probable representative
distributions) are also part of the quantum statistical derivations.
Unlike a completely degenerate Fermi electron gas where all of the
electrons are distributed into the lowest energy state for the system, the electrons
in the core region of the Sun form a partially degenerate electron gas so that they
are only sparsely distributed in the allowable phase space. Astrophysically
compact objects, such as white dwarfs (and neutron stars), can be well described
as a system of highly degenerate electrons (and neutrons) due to their
extraordinary densities, _106 glcm3 (and _1014 glcm\ The electrons in the
central region of the Sun, on the other hand, with central densities on the order of
_102 glcm3 are only slightly degenerate. Nevertheless, the effects due to this
slight degeneracy must be taken into account in the equation of state for accurate
stellar modeling [8]. Because of the large numbers of electrons in ordinary
matter, all such materials contain degenerate electrons [9].
4
An important simplification that arises in describing the electron gas in the
solar interior occurs when the gas is treated in the non-relativistic limit. This can
be calculated using the criterion kTc2 < J.... where Tc is the presently acceptedmec 30
central temperature of the Sun, me is the electron mass and k is the Boltzmann
constant, so for the solar interior
(1.38xlO-23
J / K)(1.57xlO7K) =0.0026 < 0.033.
(9. 11xlO-31 kg)(9x10 16 m 2/ S2)
Since the ratio is significantly below the relativistic criterion, the assumption that
the electron gas can be treated non-relativistically will be assumed to be valid.
The Fermi-Dirac distribution which describes the average number of
particles with quantum number f may be written in the form [10]
1(n£) = e17+jJe, + 1
where II =-~J..l, ~ =l/kT and J..l is the chemical potential. More formally, the
average number of particles in terms of the grand canonical potential, .Q, is given
by
where .QFD is obtained from the equation .Q FD (T, V, Jl) =-kBT In Z (T, V, Jl) and
the grand canonical partition function can be written as ZII (T, V) =Tr(e-jJ(H-pN»
where H is the kinetic energy operator and N is the total particle number operator
[11].
5
For a non-degenerate, non-relativistic gas, the Maxwell-Boltzmann (MB)
distribution function in momentum space is
8 2d ( 2 Jj(p)dp = 7l[J3 P exp --p-h 2mkT
where the first term on the right hand side describes the maximally allowed
occupation for the shell and the exponential term is the Boltzmann factor which
rapidly decreases as the momentum increases at constant temperature. The
number of states corresponding to the momentum in the range between p and
p + dp is proportional to the volume between two concentric spheres of radius p
and p + dp. This volume can be written to first order as 4np2dp. The Fermi
distribution in momentum space is isotropic so spherical momentum space
variables are the most natural to use, i.e., 4 7l[J3 , where the radius of this spherical3
distribution, called the Fermi surface, is equal to the Fermi momentum,
The statistical weight, or degeneracy factor, for a spin If2 system is g = 2
(since g =2s + 1), hence the term in the maximally allowed occupation shell for
the MB distribution is 8np2dp. For sufficiently low temperatures and high
densities this relationship can lead to a contradiction with quantum mechanics
when the MB distribution exceeds the limiting parabola f(p) oc p2. For systems
that tend to exceed this boundary, one says that the non-interacting electron gas is
degenerate. To guarantee that this does not happen, each quantum cell of the six-
6
dimensional phase space (x, y, z, px ,Py ,pz) must not contain more than two
electrons in which the "volume" for such a quantum cell is dpx dpy dpz dV =h3 in
the shell of momentum space (p, p + dp). In this momentum space representation,
the Pauli exclusion principle can be written in the form [12]:
This inequality follows from Heisenberg's uncertainty principle which ensures
that the density of states in the MB distribution does not rise above that required
by quantum mechanics, i.e., the electrons are forced to have higher velocity
giving them a degeneracy pressure characteristic of high density matter. In the
above inequality, the curve of the parabola gives the upper bound for the
distribution function, f(p). (See Figure 1.) If the temperature of the gas is too low,
or if the electron density too high, quantum effects must be included, so that f(p)
is forced never to exceed the parabolic upper bound -- causing the electrons there
to become degenerate.
To recover the physical particle number, i.e., the total electron density per
unit volume, the integral over the momentum states of the number of electrons per
unit volume with momenta between p and p + dp must be taken
=
ne = ff(p)dp.o
For afully degenerate electron gas, the electron number density can be
found by integrating up to a momentum cutoff (to ensure that the distribution does
not exceed the exclusion principle):
7
n - 81Z' Pf! 2d - 81Z' 3 _ 81Z' (2me )3/2e - h3 P P - 3h3 Pf - 3h3 f
o
where ne = NN and the value of £f is determined by the condition that the total
number of electrons is equal to the total number of phase space cells available. At
the absolute zero of temperature (an unrealistic, but useful assumption), the
system forms a completely degenerate gas of electrons all of which are in the
lowest possible energy state and do not violate the exclusion principle. In other
words, for a system where T = 0 K, the electrons have finite energies up to the
Fermi energy, £f, and none higher. This is depicted in Figure 2, a graph of the
distribution function versus energy which is a rectangle whose maximum energy
is £f and maximum distribution is 1, i.e., the occupation probability for Jl < £f is 1
and Jl> £f is zero. For finite temperatures (T ;j; 0), not all the electrons will be
densely distributed into the states of lowest possible momenta. This causes the
rectangle describing the occupation probability to smooth out and broaden. The
width of this transition zone broadening for finite temperatures is of the order of
the temperature. For all temperatures where the Fermi energy is equal to the
chemical potential, ef =It , the occupation index is 1/2. For systems of fermions, it
is conventional to refer to the chemical potential as the Fermi energy of the
system at a given temperature which can be defined as [14]
8
Even at absolute zero, the ideal Fermi gas pressure does not disappear since only
one electron is able to have zero momentum according to the Pauli exclusion
, 'loP 2U 2£/[1 5712
(kT2
J ] B fh o
0pnncip e, l.e., =-- =-- +-- -- +.... ecause 0 t IS zero pomt3 V 5 V 12 £1
pressure, all the other electrons have some finite momentum [15].
The number density in momentum space for a partially degenerate system
is given by the following integral
The denominator in the integrand describes a system which obeys Fermi-
Dirac (FD) statistics. Here, the electron degeneracy parameter is 11 = WkT and ~
is the electron "chemical" potential of the electron gas. In the relativistic case, the
rest energy of the particle must also be included [16]. A similar equation for the
pressure can be obtained for a degenerate non-relativistic electron gas
P = 871 =f 3V
dpe 3h 3 0 P (p) eE1kT-1] +1.
The parameter 11 allows for the gradual transition for the case of nondegeneracy to
that of complete degeneracy. In the above equation for ne, the electron number
density is a function of the degeneracy parameter and the temperature, such that
11 = l1(ne,T) [17]. This equation can be put into dimensionless form using x =
£/kT =p2/2mkT (in the nonrelativistic limit), so
9
- 41l(2mkT)3/2 =fne - 3 ------
h 0 exp(-1] +x) +1
The integral on the right hand side is known as a Fermi-Dirac integral, whose
general form is given by
Explicit solutions for the degeneracy parameter in the FD distribution law, i.e.,
(ne) = : e , are in general unavailable. (For convenience, one can approache ll+ c, +1
the problem in an alternative way by putting the integral into a general form [18]
v - 1 =f zPdp(1],p) - rcp+l) 0 e ll+z +1
d 1 · 'f h h'" . f 1 3)an so vmg It or t e cases w en 11 IS posItIve or negatIve or p =-, or -.2 2
For the case of slight degeneracy (-11 » 1), the Fermi-Dirac integral can be
2
approximated by e-ll+x + 1::::: e-ll eX where x =..!- =-p-. The FD integral may,kT 2mkT
=
therefore, be written as Fk(1])::::: ell fe-Xxkdx =ellrck +1).o
In the solar interior, where - 4 $11 $ -1 (i.e., - 11 > 0), the integral
=
Fk(1]) =ell fx ke-X[1 +exp(1] - x)r1dxo
can be expanded and integrated term-by-term to give
10
~ 1Fk (1]) =r(k + I)el] f(-1)' ( y+! erl] (for k > -1 and 11 ~ 0).
o r+I
For 11 < 0 (the applicable region for the solar interior up to RoI2), the expanded
form of the integral is [19]:
The particular FD integrals needed to describe the partial degeneracy in the solar
interior are
_ ~ I]~ ( 1)r 1 e rl]Fl/ 2 (1]) - -2e LJ - ( 1)3/2 '
r=O r +
2 _~ I]~ ()r 1 rl]-3 F312 (1]) - -2e LJ -1 ( )512 e ,
r=O r+I
Tables exist where these integrals are evaluated [20] and numerical fits are also
available [21]. More recently, numerical programs have been written which give
up to I2-digit precision for many types of FD integrals [22,23]. By splitting the
integration domain into four parts, I5-digit accuracy is also available [37].
Therefore, the equation of state (EOS) for a non-relativistic partially
degenerate electron gas in terms of the electron number density and the electron
pressure is 41Z' ( )3/2ne =-3 2mkT Fl/ 2 (1]) ,h
81Z' ( )3/2Pe =-3 2mkT kTF3/2 (1])3h
11
where m is the electron mass, k is the Boltzmann constant, T is the temperature in
Kelvin and Pe is the electron degeneracy pressure. The range of values of the
parameter 11 for partial degeneracy is - 4 ~ 11 ~ 10, but only the values between
- 4 ~ 11 ~ -1 are needed for computing the FD integrals for the Sun. In the case of
(non-relativistic) neutron degeneracy, the same EOS can be used by simply
replacing the electron mass with the mass of the neutron.
In summary, for the case of incomplete degeneracy, an additional term is
included in the Fermi-Dirac distribution, known as the degeneracy parameter, 11,
which is a function of the electron density and the temperature. The most useful
FD integrals needed to examine the effects of partial degeneracy in the Sun are
Fl/ 2 (1]) and F312 (1]). From these integrals, we can obtain the thermodynamic
variables which describe the parametrized equation of state for the electron gas in
the interior region of the Sun in terms of the electron pressure and number
density, i.e., Pe (1],T) and ne (1],T). Only the nonrelativistic degeneracy
equations are needed because of the relatively low densities and temperatures
(i.e., T < 109 K) in the solar interior [17].
Main sequence stars of lower mass have a higher degree of degeneracy.
For example, brown dwarf stars (M < O.2Mo ) have degenerate interiors. For
stars whose masses are between 5 and 8 Mo, partial electron degeneracy sets in
only after the 3 He ~ C burning stage begins, so complete degeneracy does not
emerge until after core helium runs out, i.e., when the star dies as a white dwarf.
12
For stars with masses greater than 8 Mo, electron degeneracy does not set in until
the eventuality of a supernova explosion [24]. Because the luminosity of later
stages of stellar evolution (for massive stars) is predominantly in the form of
neutrinos, the enormous energy losses they suffer greatly accelerates their rate of
stellar evolution following core helium burning.
When dealing with stellar systems where kT "" mc2, relativistic corrections
can no longer be ignored so that the integrals now take the form of generalized
X'(l+.&)'''dxFD integrals [16] Fk('l, fJ) =1 2 where ~ =kT/mec
2 is theo exp(-'l +x) +1
dimensionless temperature and the EOS for degenerate, relativistic electrons is
81i,fi 3 3fJ3/2 [ fJ R1;' fJ ]ne =--3-meC Fl/2 ('l, ) + jJL 3/2 ('l, ).h
16,fi 4 SfJS/2[ fJ fJ fJ ]Pe =-3-meC F3/2('l, )+-FS/2 ('l, )3h 2
The effects of degeneracy and relativity act in opposition: at high temperatures,
the relativity correction becomes important while the degeneracy parameter
decreases, and vice versa. These equations find applications for stellar systems
such as white dwarf stars and stars undergoing supernova core collapse.
13
2.0 The MSW Effect
Brief Overview
Electron neutrinos created in the energy generating solar core through
thermonuclear fusion reactions scatter with ambient electrons in the solar plasma
as they pass through the Sun's interior. Depending on their energies, the ambient
density where they are produced and the electron density gradient they encounter,
these newly formed electron neutrinos - which are coupled to the electrons
through the electroweak interaction - can transform into other flavors through the
effects due to charged-current interactions.
The addition of the charged-current Hamiltonian, HM , into the time
dependent propagation equation i d If! = (H 0 +H M Nt allows for the possibility ofdt
flavor conversion. Mass differences arise in the mixture of the neutrino mass
eigenstates -- through forward scattering of the electron neutrinos with the
background electrons -- as they propagate through inhomogeneous density
regions in stars and planets. The existence of massive neutrinos permits quantum
mechanical neutrino oscillations to occur in both vacuum and in stellar and
planetary interiors. With the inclusion of this added mass term, the neutrino mass
eigenvalues in matter are found to be functions of electron number density and
neutrino energy:
14
When the resonance condition is met, i.e., A :::: !1 cos 2B =2.fiOF neEv where
Ev is the neutrino energy,!1 =m; -m12 and OF is the weak interaction coupling
constant, the values of the mass eigenvalues in matter, iii;, change gradually as
they propagate through the solar interior as long as the electron density gradient
drops off sufficiently slowly, i.e., adiabatically. What this means physically is
that the neutrino mass eigenstates have sufficient time/distance to adjust to the
changing density of electrons. This density dependence can be made more
explicit by noticing that the matter mixing angle is a function of the electron
number density and the neutrino energy, 8M =8M (ne, E) where ne=ne(x). These
density dependent variables change as the electron neutrinos make their journey
from the region of their origin to the solar surface. Most importantly, however,
the mass eigenvalues change in accordance with the changing electron density
profile they experience. In the case of constant density, the neutrinos undergo
oscillations similar to those for vacuum but with altered mixing angles and
oscillation lengths.
Consider the graph of the mass eigenvalues in matter squared versus the
electron number density profile of the Sun. (See Figure 3.) For adiabatic changes
- those that occur slowly enough for the electron neutrinos to match the changing
density of the surrounding electrons - no "level crossing" takes place and the
electron neutrinos that travel from regions of greater to those of a lesser density
15
are gradually converted into mu- or tau-neutrinos after passing through a critical
density region. When the neutrino conversion takes place through level crossing,
the change occurs abruptly in a manner similar to quantum mechanical tunneling.
In the case when the electron neutrinos originate in a region with high
electron density, they interact so strongly with the ambient electrons that mixing
is suppressed so they are essentially in the high mass eigenstate, i.e.,Iv2) :::: Ive) .
When the critical density is reached (where the level crossing separation is
minimal), maximal mixing occurs and, after passing through the critical density
region, the original high mass eigenstate electron neutrino is transformed into
another flavor, i.e., Iv2 ) :::: IVa) with a transition probability proportional to cos2 8.
The above follows directly from the fact that mass eigenstates of massive
neutrinos can be represented as a linear combination of flavor states and because
the mixing angle in matter is a function of electron density.
Since the exclusion principle constrains the number of electrons per unit
cell that may exist in phase space (causing the phenomenon of electron
degeneracy), the electron density profile - one of the critical parameters allowing
for the occurrence of neutrino flavor conversion in matter - is altered. This study
will examine the extent of this variation in the gradient of the electron number
density as the electron neutrinos pass through the solar core and exit the surface to
see how the altered electron density profile (due to the electron degeneracy)
influences the adiabatic conversion of Ve -7 Va via the MSW effect.
16
2.1 The Interaction Hamiltonian
Charged current electron neutrino-electron forward scattering gives the
electron neutrino a refractive index through its interaction with the ambient
electrons in the solar plasma which can cause a fraction of the electron neutrinos
created in an interaction state to undergo resonant flavor conversion. Because
only the electron neutrinos are affected by both the charged- and the neutral
current interactions, they acquire a different index of refraction as they propagate
in the solar medium than either the mu or tau neutrinos which interact solely
through the neutral current weak interactions. The differences in the refractive
indices between Ve, vI! and V1: lead to different phases as the various types of
neutrinos pass through the solar interior which can lead to flavor conversions
under the suitable conditions.
The charged-current interactions that take place between the electron
neutrino and the ambient electrons in matter are mediated by the charged vector
bosons, Wi. (See Figure 4.) Through this boson exchange process, the electron is
transformed into a neutrino and the neutrino transformed into an electron. Owing
to the low energies associated with these processes taking place in the solar
interior « 20 MeV), the interactions can be thought of as occurring
instantaneously, so that the terms describing the formation and destruction of the
Wi vector bosons (- 80 GeV) do not need to be included in the Hamiltonian.
17
The effective Hamiltonian that describes such low-energy ve-e scattering
processes is given by the Glashow-Salam-Weinberg (GSW) theory in the
Standard Model (SM)[13]. It has evolved over the decades since the four fermion
interaction was first described by Fermi in 1933. In analogy with
electrodynamics, the total effective weak interaction (WI) Hamiltonian can be
written as [25]
where J~ represents the charged currents and K~, the neutral currents and p = 1 in
the GWS theory. The current-current hypothesis says that weak processes take
place through the interaction of the current with itself, i.e., H weak = ~ J /J; and
that universality is result of this weak current self-interaction [26]. In terms of the
quark and lepton Dirac spinors, the charged four-current can be explicitly
represented as [27]
where Y~ and Ys are Dirac gamma-matrices and K+ is the CKM (Cabibbo
Kobayashi-Maskawa) quark mixing matrix. The CKM matrix arises because the
massive quarks' mass eigenstates are not the same as the WI eigenstates - there is
a mismatch between the mass eigenstates and the flavor eigenstates [28]. The
value of the weak Fermi coupling constant in the weak Hamiltonian is found
18
experimentally from muon decay measurements to be OF =1.16637 X 10-11
(MeVr2. (Since the coupling constant has the same value for allieptonic weak
interaction processes it is said to exhibit the property of universality which is of
importance to grand unified theories.)
The components of the weak leptonic current can be expressed in the form
J;(x) =Jl (x) +Jf(x) +Jl (x).
For electron-neutrino scattering (Figure 4), the electronic component of the four-
current is given by [29]
where e and ve are adjoint and Dirac spinors, respectively. In the above
equation for Hweak, J; can be found by taking the hermitian conjugate of the
electronic component of the four-current, i.e.,
where Y; =Ys' Since v; =veYo and Y; = YoY,uYo, the above can be rewritten as
J(e)+ - (1 ),u =veYo - Ys YoY,uYoYoe
Finally, because YoYo =1 and Ys anticommutes with all y-matrices [30], we obtain
J (e)' - - (1 ),u - veY,u - Ys e.
So, ignoring the neutral current interactions, the effective weak Hamiltonian
becomes
19
where PI, P2, P3 and P4 are the momenta of the respective leptons (Figure 4).
Following a Fierz transformation (Appendix A), the matter interaction
Hamiltonian takes the form
exhibiting its vector minus axial (V - A) coupling since veY/Ye is a polar vector
bilinear and veYfJ Y5V e is an axial (or pseudo) vector bilinear.
, (1 0)In the Dirac field (as opposed to a chiral, or Weyl, field), yO = 0 -1
and y, =iyoy' Y'Y=(~ ~). In this representation the term (I . y,)l2 is the
projection operator which projects out only the left-handed neutrino and
(1 + Ys)12 is the projection operator for the right-handed neutrino. In the
expression.! (1 - Ys)\If, \If represents a Dirac spinor for either the neutrino or the2
electron which is a four component system. For example, the lepton spinor in the
chira! representation is written in column vector form, Le., 'If =(~:) where
If/L.R =(:e) .However, because the ve-e scattering is a V-A interaction, onlya L.R
20
the left-handed currents undergo interactions described by the above Hamiltonian
[25].
After averaging over the electron field bilinear in the case of forward
scattering (i.e., pz = P3 = p), the effective interaction Hamiltonian becomes
HM =2.fiGFVe(P)Y/Ye (p)(eylJ (l- Y5)e)
where (l - Y5) has reduced to a value of 2 because the neutrinos are left-handed.
In the nonrelativistic approximation, the axial current reduces to spin so its
contribution is negligible for nonrelativistic electrons consequently only the Jl =0
term contributes [31]. Therefore, the average over the electron terms can be
condensed to (e yOe) == (e+e) == ne. In the rest frame of the electron, the
interaction matter Hamiltonian can now be rewritten as
where the electron neutrino-electron interaction potential is V = .fiGFne' This
term describes coherent forward scattering of the electron neutrinos with the
ambient electrons which allows the MSW effect to occur under certain conditions.
Because of the unequal scattering between the electron neutrinos (via charge and
neutral current interactions) and the other flavors (via neutral current
interactions), the electron neutrino gains an effective mass (or refractive index)
which neither the mu or tau neutrinos do since they only interact through neutral
current reactions mediated by the neutral intermediate boson, Zoo (See Figure 4.)
21
2.2 Two neutrino vacuum oscillations
There are three (3) known generations of quarks and leptons, so there are
likewise three (3) electroweak flavors of left-handed neutrinos: Ve, vI-! and v'(;.
Since there are three generations of neutrino flavors, there are three mixing
angles, two mass-splittings, and a phase factor associated with CP violation in the
neutrino sector. Some four (4) neutrino models have been proposed where the
fourth neutrino is a non-weak interacting "sterile" neutrino [32], vs, i.e., the
interactions are not mediated by standard model gauge vector bosons so they are
not physically measurable (or only very weakly so).
In what follows, vacuum neutrino oscillations will be examined with
the simplifying assumption that there are only two species of neutrino: the
electron neutrino, Ve, and either a mu or tau neutrino, represented as Va where a
stands for either Il, or't. Neutrino flavor eigenstates composed of a superposition
of mass eigenstates allow for the phenomenon of neutrino oscillations. Vacuum
oscillations are a result of quantum mechanical interference where different mass
eigenstates propagate dissimilarly, leading to changes in the flavor eigenstate over
distance or time.
Since we do not know the physical origin of mass [33], there is
nothing which requires weak interaction (or, flavor) eigenstates to be the same as
their mass eigenstates. To see this, imagine that the initial flavor eigenstate is a
superposition of mass eigenstates as represented by a Dirac ket, or state vector
22
which evolves in time as IVa)t =ViVa) where V is the time evolution operator,
V =e- il1t• When the Hamiltonian operatorH acts on the eigenvectors Ivk ),
written more generally as IVa)t =ei(P'X-Ekt)lvk ) where the various components of
the 3-momentum are assumed to be the same whereas the energy components, Ek,
are not. However, for highly relativistic neutrinos, because the phase factor is
Lorentz-invariant in the lab frame, it does not matter whether the neutrino is
formed with definite momentum or definite energy [34].
Massive neutrinos travel with speeds approaching that of light, so
the energy eigenvalues in the ultrarelativistic limit are given by Ek =~ p2 + m: .Here, natural units (Ii = c = 1) have been used, and p represents the neutrino
momentum (i.e., p = Ii k), and mk, the mass eigenvalues. For large momenta and
small neutrino masses, the expression for the energy can be approximated using
the quadratic expansion
where p ::= E for nearly massless neutrinos. The significance of the above
equation relating mass eigenvalues, neutrino momenta and energy eigenvalues
follows from the fact that different mass eigenstates are able to acquire different
23
phases as they propagate in vacuum. This can be seen more easily by rewriting
( m~) 2 (mb )-i p+ 2£ t _i mkt - 2ithe flavor eigenstates as e as e 2£, so that IVa (t)) = e Ivk). The
e-ipt term has been dropped because it only adds an uninteresting phase factor, i.e.,
a constant term to each neutrino flavor state vector.
Because neutrino flavor eigenstates can be represented as a linear
combination of mass eigenstates, the probability for an electron neutrino to
transform into another flavor can be obtained from the squared modulus of the
transition amplitude
or more explicitly
m2t-i-
P(ve~ va) = IVeke 2£VC:k
2
In the case of just two Dirac neutrinos, U describes a rotation matrix where
(
COS e - sin eJU = . and the mixing angle, 8, is the parameter that relates the
sme cose
(Ve (O)J (cos e - sin eJ(vl (O)Jflavor eigenstates to the mass eigenstates, i.e., =. .va(O) sme cose v 2 (0)
From the transition probability equation, it can be seen that the neutrinos can have
significant mixing if their masses are nearly equal, so that if the difference
between the masses is small, the exponent will be correspondingly large. It has
been assumed that the neutrino mass eigenstates are stable [35], i.e., they do not
24
decay, so that the time evolution of the initial state can be represented as
IV/(t») =Le-iEktV;klvk); otherwise, decay terms such as e-n must be includedk
where r is the decay constant. Weak flavor eigenstates can be written as a linear
combination of two (2) mass eigenstates at time t = 0 as
Ve(O) =vl(0)cos8 - v2(0)sin8
Va(O) =vl(0)sin8 + v2(0)cos8
Here, the vacuum mixing angle, 8, parametrizes the degree of mixing,
assumed to be non-zero for unequal mass eigenstates, so that the mass eigenstates
are nearly degenerate, but ultimately non-degenerate. In addition, as the mixing
angle relates various eigenstates, it cannot be time-dependent. Instead, the way
that the mass eigenstates vary with time is represented as !vk(t») =e-iEktlvk(O)). In
other words, each mass eigenstate behaves as a free parameter with energy Ek, so
U is the rotation, or mixing, matrix, then the mass eigenstates can be expressed in
terms of their flavor eigenstates at time t = 0 as
(VI (0)) (cos0 sin 0)( ve (0))v
2(0) = -sinO cosO va(O) ,or
25
V2(0) =-ve(0)sin8 + vu(0)cos8
It should be emphasized that, although Verepresents a neutrino produced in a
charged-current interaction, it is not a physical particle; instead, it is a
superposition of physical fields made up of VI and V2 which have dissimilar
masses, Le., VI and V2 represent different physical mass eigenstates.
Substituting these expressions into the time dependent electron neutrino
eigenstate gives
Rearranging in terms of flavor eigenstates at t =0, the equation becomes
Ve(t) = (e- iEjl cos28 + e-iE21 sin28)ve(0) + sin8 cos8 (e- iEtl- e-iE21 )vu(O) where
vu(t) = e-iEtl vI(0)sin8 + e-iE21 v2(0)cos8.
The transition amplitude for an electron neutrino (at time t = 0) to
transform into either a mu or tau neutrino at time t is
26
and (Ve (0)IV e (0)) = 1, (Va (0)IV e (0)) = 0 because the eigenstates are orthonormal,
Therefore, the transition probability is
Since 2 cos8Et = eitilit +e-itilit, then P(ve ~ va) = 2sin 2 Bcos2 B [1 - cos8Et].
Using the trigonometric identity sin28 =2sin8cos8, this can be rewritten as
The argument to the cosine term can be put into a more physically
revealing form by letting L represent the distance the neutrino travels from the
location of its origin to the detecting apparatus. Because the neutrinos are
relativistic (and c =1), L =1. Using the relativistic approximation, the energy
difference ~E =Ez - E1 can be written as
~2 n: (m
2- 2J ~m2 ~m2M= p 1+-2 - P 1+3-:::: p 2 m,. =--. Using M::::-- and
2p2 2p2 2p2 2p 2p
t =L, the transition probability is given by P(ve ~ va)=!:.sin22B(I-cos ~m2L)2 2£
where pv :::: Ev for nearly massless neutrinos. Finally, using the trigonometric
27
· . . 2 1( ) 11m2L 11m
2L h ..IdentIty sm ¢ =- 1- cos 2¢ where 2¢ =--, and ¢ =--,t e transItIOn
2 2£ 4£
probability for an electron neutrino to rotate into another flavor is given by
pry, -->va )=Sin 2 2{/Sin 2( ";;L)-
In terms of the physically measurable electron neutrino survival probability, we
find
In this form, the Ve survival probability is a function of the neutrino oscillation
parameters, 11m2 and sin2 28, the distance from source to detector, L, and neutrino
energy, By.
28
2.3 Neutrino Flavor Conversion in Matter
As Pontecorvo [36] first pointed out in analogy with the system of
oscillations in the quark system of neutral K-meson oscillations, massive
neutrinos may also undergo oscillations [108] from one flavor to another in the
system of neutrinos and antineutrinos. An analogy exists between the vectors of
the neutrino mass eigenstates Ivl ) and Iv2 ) and the state vectors IK J and
IKs ) which describes KL and Ks, i.e., particles with definite mass and width, and
the neutrino flavor eigenstates Ive ) and Iv,u) as analogues of IKo) and IKo)' i.e.,
vectors that describe particles with definite strangeness, i.e., K o and K o [38].
The difficulty, however, with attempting to explain the solar neutrino problem via
vacuum oscillations is that the oscillation lengths, which are on the order of
hundreds of kilometers, require mass splittings that are too small by many orders
of magnitude. When neutrinos propagate in matter, however, the mass matrix is
modified because of changes in the various neutrino effective masses brought
about through the disparate interactions each flavor in the medium individually
experiences leading to greatly reduced oscillation lengths.
When electron neutrinos encounter the ambient electrons in the solar
interior, they interact via charged- and neutral-currents. Since v~ and v" only
interact with electrons through the neutral-current reactions, their interactions
with the background have different magnitudes than those for Ve• Therefore, the
29
effective mass of the neutrino is modified while passing through matter in such a
way that the modulation of the Ve component is different from what it would be in
vacuum. This difference causes a distinct change in the oscillation probability of
the emerging electron neutrino in matter producing modification in the oscillation
length and mixing angle in matter analogous with that in vacuum.
In his derivation of the matter dependent neutrino propagation equation in the
two-flavor model [39], Wolfenstein showed that the electron neutrinos - in their
charged current interaction with the ambient solar electrons - have different
refractive indices than the other neutrino flavors.! In this optical analogy, vJ..l and
VT do not interact through the charged current JJ..l mediated by the intermediate
boson, W, so that there is a difference in the respective Ve and Va refractive
indices,8n. The interaction with matter adds an extra energy/mass term, VO, to
the energy momentum relation
where the refractive indices, nj, appear in the time-dependent state vector
IVe)t =I \vj)ei(nikox-Et).j
I From the solution of the extinction theorem, the index of refraction of a gas is found to be
n =1+2n A2Nf(0) where N is the number density of atoms and f(O) is the forward scatteringamplitude per atom [40]. The refractive index for (anti) neutrinos in matter is n =1 ± GFN(3ZA)/Ev-V2 [41].
30
The dispersion relation in matter has an added energy term and k 7 k' =
nk where n is the index of refraction and VO is the time-like component of the
four-potential, V''\ in the nonrelativistic limit, where k'2 =£,2 _m2, so
Neglecting second order terms in V,
Substituting in E2=k2+ m2gives
(nk)2 "" k2- 2EV,
so
where for potentials in ordinary matter, V =.J2GF ne • In other words, a change in
phase is associated with an index of refraction of the various types of neutrinos
traveling through matter where the index of refraction is given by the optical
theorem, i.e., ken-I) = 2nNf(O)/k where k is the neutrino momentum and N the
density of scatterers, thus [42]
For non-ordinary states of matter, such as those formed during the extreme
temperatures of the early universe and during core collapse of massive stars,
higher order terms in the potential are kept [43].
31
The difference in the refractive index in the case of the electron neutrino
and the other flavors is ~n = 7.6 x 10-19 ( P 3)( E ). Although this is100g/em lOMeV
indeed a small value, it leads to significant differences for those in vacuum if the
neutrinos have non-zero masses [44].
By bringing together the spatial phase shift for the induced refraction of
the neutrinos in the solar medium with the temporal phase shift from the mass
matrix in vacuum, Wolfenstein was able to describe the change in vacuum
oscillations in matter caused by the differences in the effective masses and indices
of refraction of the neutrino interactions with the ambient solar interior through
charged and neutral current electroweak interactions [45].
2.4 The Neutrino Propagation Equation in Matter
The Klein-Gordon (KG) equation is a relativistic propagation equation for
spinless particles with mass and can be represented in the form
Since the weak interaction only couples to the left-handed components of the
neutrino field, the spin structure from the wave equation may be eliminated so
32
that the KG equation can now be written compactli in the basis of neutrino mass
eigenstates as
To solve the KG equation for the case of a linear combination of various mass
eigenstates, it will be assumed that all neutrinos have the same 3-momenta so that
the differential operator d2
2 , proportional to the identity matrix, can be droppeddx
because it only introduces indistinguishable and unmeasureable phases.
Additionally, by specifying a particular neutrino direction and substituting in
Iv(t») =e-iE1Iv) , the reflected solution can also be ignored, leading to the first
order differential equation [49]:
which is a Schrodinger-like wave equation with the solutions of the form
° ](V1(O)] B " . h h D' . h'E • egmnmg WIt t e Irac equatIOn, t ee-121 via)
propagation equation obtained in matter is [39]:
In the interaction basis, the potential term in the mass matrix is diagonal
2 Rigorous derivations of MSW formulae have also been made beginning with the Dirac equation[45-48].
33
which becomes (Appendix E),
where 2.fiOFneEv ' This evolution equation holds for the propagation of either
Dirac or Majorana particles where the mass matrix in the case of constant density
is determined by adding an induced electron neutrino mass term (A = .fiOFneE)
to the mass squared matrix in vacuum, i.e., M 2-7 M 2 + A (Appendices D&E),
so
i~(:eJ=_1(- ~:OS28+ A ; sin 28J(:eJ.dx f-l 2E -sm28 -cos28 f-l
2 2
The matter-mixing angle, which controls the oscillation probability, is
obtained from the trigonometric relation
tan 28M
= sin 28M = 2(HM )12 = li sin 28cos 28M (H M ) 22 - (H M ) 11 li cos 28 - A
It can also be recast into an equivalent, but more telling form
. 2 28 _ li2
sin 2 28sm M - ( )2 .
licos 28 - A +li2 sin 2 28
This equation is of the form of a resonance equation, such as that of Breit-Wigner,
where the resonance half width is rt2 = lisin28. This equation describing the
34
mixing angle in matter shows the degree of mixing between the linear
combination of flavor states upon creation, while propagating through the
resonance region and as it emerges from the solar surface. (See Figure 31.)
As the mass eigenstates propagate, they each acquire a different phase;
yet, they are not the states that are produced or detected through the weak
interaction. Instead, the physical quantities one observes during neutrino
production and detection are the flavor eigenstates because of the weak
interaction processes of neutrino creation and destruction. It is the
parametrization in terms of the rotation (mixing) matrix that allows the neutrino
mass eigenstate solutions to be described in terms of the neutrinos that are
produced and detected. However, it is generally believed that it is not Ve and vI!
which propagate in space but, instead, VI and V2 [50].
35
2.5 Propagation Equations for Homogeneous Densities
In the case of vacuum oscillations, the evolution equation can be written as
. d (VI (t») (VI (t»)1 dt V
2(t) =H v
2(t)
where H is diagonal in the basis of mass eigenstates, i.e., H = ( ~' 0) andE2
2
Ek :::: p + mk represents the energy eigenvalues in vacuum. In the flavor basis the2p
equation is
I + m l2 + m~ m~ - ml
2(-COS28
where H =UHU =P + + ---=---=-4p 4p sin 28
and the mixing angle is given by2H'
tan 28 = 12
H'22-H 'l1
sin 28) (Appendix D)cos 28
The evolution equation for neutrinos propagating in matter modifies the
above equations, so that
where
-~cos28+J2GFne4p
~sin284p
~sin284p8
-cos284p
36
and H M =V =.[iGFne in direct correspondence with the equation for vacuum
oscillations. In other words, under a unitary transformation using the matrix U
which connects the mass and flavor eigenstates, the evolution equation takes the
above form. The effective mixing angle in matter, 8M, is now given by
2(H ) ~sin28tan 28 - M 12 =-----M-
(HM )22 - (HM)l1 ~cos28- A
where A =2.[iGFneP and ~ =m; - ~2 , again, in direct analogy with the
equation for the case of vacuum oscillations. The effective mixing angle is a
function of the electron density and A is related to the induced effective mass
, ~cos28when resonance occurs as A = ~cos28, or ne = J2 since
2 2GFP
Expressing the corresponding mass eigenstates in matter for the case of
constant density in terms of their respective flavor eigenstates can be obtained
through the analogy with the transformation equation for vacuum oscillations
where the equations for the case of homogeneous density are identical to the case
of vacuum oscillations except now VI ~ (vM )1 and 8~8M. Thus -- with the
appropriate modifications -- the behavior of electrons propagating in
homogeneous density matter is the same as in vacuum, i.e., no resonance
modifications occur for neutrinos traveling through media with constant density.
37
2.6 Neutrino Flavor Conversion in Media withNonhomogeneous Densities: The MSW Effece
One of the important things to keep in mind when dealing with neutrinos
propagating in media with nonhomogenous densities is that the mass eigenstates
are no longer eigenstates of the Hamiltonian, so that instantaneous solutions in the
adiabatic approximation are sought. For convenience we will use a more
abbreviated notation, where IfF! ~ (~:), so the flavor evolotion equation is now
. d 1 M 2l-lf/ =- If/.dx f 2£ f
O2J'the interaction evolution equation becomes
M2
where UM = UM(X), so (Appendix E):
where the second term on the right hand side accounts for the inhomogeneous
density. In the case of homogeneous density the differential term does not appear.
In the above equation, UM is the mixing matrix in matter
1 This section is noticeably indebted to T.K. Kuo and 1. Pantaleone, "Neutrino oscillations inmatter," Rev. Mod. Phys. 61 (1989) 937.
38
(
COS 8MU =M . 8sm M
and U~ its Hermitian conjugate. The off diagonal terms in the matrix of the
mass eigenstate evolution equation are what cause the states Ivl ) and Iv2 ) to mix,
where the interaction should be thought of in terms of instantaneous mass
eigenstates:
The adiabatic condition for the phenomena of matter enhanced oscillations
can be obtained by starting with the adiabatic inequality -- 0E8t» n-- in terms
of the energy gap between the levels, 8E, and the time of transition where the
neutrino is in the level crossing region, 8t [ref. 44, p. 106]. The energy gap can be
obtained using the relativistic approximation to the energy difference equation
m 2 _m2 11where I1E::::: 2 I and, so OE - -·-sin 28. The density gradient is
2p 2E
.!!- (In ne ) =~ dne ,so the inverse of the transition time between the gap can bedr ne dr
written (as r ~ t and d - 8) as ~ =~ dne~ - (~ dne)~ where A =I1cos288t ne dx &Ie ne dx M.
at resonance so 8A -l1sin28 (the width of the resonance). Since OE =~sin 282E
39
d e (1 dne J-1
8sin 28 h ' h' I' +' han at = --- ----, t en usmg t e mequa tty lor t e energy gapne dx 8cos28
8£& »1 (since tz =1), we obtain
8 . 28( 1 dne J-1
8sin 28 1-sm --- » .2E ne dx 8cos28
The adiabatic condition at resonance is often written in the form (y» 1) where
8sin 2 28y=---.,.....-----,-
2Ecos28~dne
n dxe res
therefore, leading to a negligible hopping probability, since
and for large y, Phop -7 0
The formula for the electron neutrino survival probability is given as [51]
where PLZS is the Landau-Zener-Sttickelberg transition probability and 8~ is the
mixing angle in matter at the point of production. When the above adiabatic
condition holds (i.e., y» 1), then the transition probability, the probability for a
neutrino on one of the trajectories to jump to the other trajectory in the level
crossing diagram, becomes negligible, soP(ve ~ vJ =~(l + cos 28~ cos 28) ,
40
independent of whether the neutrino passes through the resonance or not [ref. 27,
p.950].
Whflt this means in terms of the allowed parameter space for neutrino
oscillations (~ vs. sin2 28) in the Sun, is that the diagonal, nonadiabatic region can
be eliminated. (See Figure 5.) Recent results from KamLAND in combination
with solar neutrino data, have found that the small mixing angle (SMA) solution
and the LOW ~m2 region can also be excluded leaving the large mixing angle
(LMA) region on the MSW plot as the leading solution to the solar neutrino
problem. From analyses of solar, atmospheric and reactor neutrino experiments
the following neutrino oscillation parameters for 10' allowed ranges are found [3]
tan 2 8 =0 41+0.0812 • -0.07
sin 2 2823 > 0.92
tan813 < 0.16
As the effective mixing angle in matter determines the oscillation
probability, P =P(8M), the mixing angle in matter, 8M , in tum, depends on the
electron number density and energy at a given point, i.e., 8M =8M (nix),E).
Therefore, the propagation equation describing mass eigenstates in matter
represents the Hamiltonian changing adiabatically from point to point. In this
situation, the vJ.L fraction of the propagating wave packet has sufficient time to
41
build up as long as the resonance condition is met, Le., cSt =cSx »Lose. At
resonance, the hopping probability - the probability for one eigenstate to jump
abruptly to another eigenstate - for the solar interior is negligible since the density
varies gradually enough to fulfill the adiabatic condition. In other words, if the
density term varies sufficiently slowly so that the oscillation length is of the order
of one wavelength in matter, then the off diagonal terms in the mass squared
matrix may be ignored and IVI) and Iv2) become instantaneous mass eigenstates
of the Hamiltonian.
In the case of a medium with an inhomogeneous density profile, 8M
depends on the gradient of the electron number density as well as the neutrino
energy (in the sin2 8M equation) [53]. The propagation equation in the mass
eigenstate basis in matter can be written (Appendix E) as
d8M 1 Llsin 28 dAwhere - =- ( )2 ( )2 [ref. 27, p. 949], or
dx 2 A - Ll cos 28 + Ll sin 28 dx
more explicitly in terms of electron number density [49]
42
In the case where there is no density variation (Le., where the electron number
density is constant), then d8M = dne =0 and the system of equations reduces todx dx
that of the stationary state analogous to the case of vacuum oscillation where
The radial density inhomogeneity variation in the solar core gives rise to
the possibility of resonance conversion when the adiabaticity condition is
fulfilled, i.e., 181« 1m; - m;l. Under these circumstances the Hamiltonian can be
defined at a given point, i.e., the matter eigenstates pass through the medium with
a constant relative mixture of Ve and vJ..l at a given point. The oscillation length at
resonance is L = 47tE which is the scale on which the interference occurs.res 8sin 28
In this case, the vJ..l fraction of the propagating wave packet in Ve has sufficient
time to build up (i.e., 8t =ox), or distance over which to match the slowly
changing density as long as the resonance condition, Ox » 4es, is satisfied.
When the traveling electron neutrino enters the resonance region of the Sun
(-Ro/5), the flavor of the complete state, Le., Vz, matches the changing density, so
that a non-oscillatory flavor transition takes place because of the mixing between
the mass eigenstates, VI and Vz [54].
At the surface of the Sun, the electron survival probability is
approximately equal to sinze which gives it its characteristic non-oscillatory
43
transition probability. Due to the fact that solar neutrinos have a relatively short
coherence lengths, - 10-6 cm, having been created from rapidly oscillating nuclei
in the hot solar core [55], the neutrino mass eigenstates will be incoherent so
phase information will be lost, leading to a classical probability. In this case, the
oscillatory term will be averaged out, so
Thus the neutrinos travel from the core of the Sun, pass through the narrow region
in which the effective mass enhancement occurs (as some mixture of Ve and va)
and exit from the solar surface and travel to the Earth relatively unchanged from
the state acquired upon leaving the solar surface [56].
Depending on the initial energy and the point of neutrino origin there are
three neutrino energy regimes: 1) below 2 MeV (i.e., the energy region with
which most of the neutrinos are formed in the pp reaction in the Sun), where there
are only small matter corrections to the vacuum oscillations; 2) between 2 MeV
and 10 MeV, where there is a noticeable non-oscillation contribution in addition
to the oscillation effect; and 3) above 10 MeV, where the non-oscillatory
adiabatic effect dominates (along with some small oscillation effects). The
measured average probability is somewhat higher than that expected from a pure
sin2enon-oscillatory term alone which may be attributed to the effects of
44
hypothetical sterile neutrinos,2 whose overall effect is one of a completely non-
oscillatory matter effect for certain values of the mass difference [ref. 54, p.16].
When the adiabatic condition is valid, the mass eigenstates can be
considered instantaneous eigenstates of the Hamiltonian, so that the linear
describes the state of the neutrino at a given point of constant electron number
density. In conjunction with this fact, the level crossing diagram and the mixing
angle in matter versus the electron number density diagram portray the behavior
of the neutrinos when they are created in the solar core, propagate through the
critical density region (provided that they have a sufficient energy), and exit from
the solar surface. (See Figures 3 and 32.}
When an electron neutrino is first created in the Sun, it finds itself in a
region where the electron density number is significantly greater than at
resonance, i.e., ne »n;es. From the diagram of the matter mixing angle versus
density, it can be seen (Figure 32) that the matter mixing angle is at its greatest
value (8M ::::: n ), and the electron neutrino is primarily in the high mass2
eigenstate, i.e., !vz)::::: Ive ). At this point the mixing length in matter is given (in
analogy with that in vacuum) as LM = 4nE (where /).. M =m~ - mlz) which is
/)..M
much less than that in vacuum -- making the MSW effect physically significant.
2 Alternatively, the larger than expected survival probabilities may be due to density fluctuationsin the solar core [57].
45
When the neutrino enters the region where ne =n;es , the mixing angle in
matter is such that maximal mixing occurs, i.e., eM =n, where equal amounts of4
the two flavors (in the two flavor model) make up the mass eigenstate of the
propagating neutrino.
Finally, as the neutrino reaches the solar surface, where ne «n;es , the
. . 1 . ... . l' e 0 h L 4nE hmlXmg ang e m matter IS at ItS mmlmum va ue, I.e., M = were =--, t e~
same as that in vacuum and Iv2) =IVa) .
If an interaction does occur between Ve and Va (i.e., e "# 0), there is no level
crossing and the levels repel each other. The nature of the level crossing can be
understood in terms of a state system where the energy levels are a function of
some parameter, such as an external magnetic field which changes slowly.3 When
A =~cos28 =2.J2GFneEcrit ' the distance between the levels is a minimum. If a
neutrino is created in the Sun with E > Eerit (or P > Perit) then the Ve appears on the
upper right hand comer of the level crossing diagram. (See Figure 3.) As the
neutrino passes through the Sun toward the surface, both the electron density and
the magnitude of the resonance parameter, A, decrease. If this decrease takes
place slowly enough such that the adiabatic criterion holds, the neutrino's
trajectory corresponds to the upper curve where the neutrino is made up of a
linear combination of flavor eigenstates. Thus, an electron neutrino that is created
3 The crossing point can be viewed as a diabolical point whose collective point always tries to goas far as possible from the point of degeneracy, as a charged particle in a magnetic monopole [58].
46
in the high-density region of the solar interior will arrive at the solar surface as a
higher mass eigenstate neutrino, i.e., Iv2 ) with a reasonably high probability of
being in a non-electron neutrino momentum state, i.e.,Iva)'
The above argument follows from the adiabatic theorem which says that if
the newly-created neutrino begins on either of the two trajectories, then it will
continue on that trajectory as long as the density changes adiabatically; otherwise
a level crossing will occur with the probability given by Phop . Because the
neutrino mass matrix is a function of the solar density, the mechanism whereby
the density effects the neutrino mass is due to the differences in the nature of
scattering that the various neutrinos experiences as they travel through the
resonance region. If the density that the neutrinos are passing through is constant,
then the flavor eigenstates in terms of the mass eigenstates may be written
explicitly as
where (}M is defined through the equation tan 2(}M = sin~ . When
2() 2 2GF ne Pcos + -2 -2
m2 -m1
ne = 0, then 8M = 8 and the flavor eigenstates are the same as the mass eigenstates.
If m2 > mt and the density is very large and ne ~ 00, then lim (}M (ne ) -7 1l andne~OO 2 .
47
so every neutrino produced as ve (at a density greater than the critical density) will
be primarily in the heavier mass eigenstate, i.e., Ive(ne)) =:: Iv2 (ne)) where an
equality holds when ne ~ 00.
The critical resonant solar neutrino energy is given by [ref. 59, p. 263]
(11m
2 JEcrit =6.6cos8 10-4 eV 2 MeV
and the corresponding critical density, where 8M (n;rit) = 7r , is [ref. 59, p. 262]4
In the case of the Sun (using the combined results from KamLAND and the solar
neutrino data) the resonant energy is about 4 MeV with a critical density between
90 glcm3 (O.IRo) and 10 glcm3(- O.3Ro). Thus, the neutrinos emitted in the
boron-8 (and hep) reaction(s) will have sufficient energy to pass through the
resonant region and convert to one of the other generations on its way out of the
Sun. The extent of flavor conversion also depends, however, on the distance
between where the neutrino originates and where the resonance takes place, so
that the point where the neutrino is produced (in terms of electron density)
determines its initial degree of mixing [ref. 54, p.12].
48
Summary
Neutrino propagation in matter is governed by the matter wave equation
which can be obtained from the Klein-Gordon equation. (Alternatively, one can
use the Dirac equation via field theory.) The neutrino mixing angle in vacuum is
similar to the Cabibbo angle for the analogous system of quarks where the quark
mixing matrix, known as the Cabibbo-Kobayashi-Maskawa (CKM) matrix, arises
because the quark mass eigenstates are not identical to their weak interaction
eigenstates. Since there are no fundamental symmetries to prevent the neutrinos
from having mass, the existence of massive neutrinos does not violate any known
conservation laws, i.e., the existence of massive neutrinos only requires a minimal
extension of the SM.
When a neutrino is produced via the weak interaction it is in an interaction
eigenstate and afterwards it propagates through the medium in a superposition of
mass eigenstates. Since the flavor and mass eigenstates are not in general the
same, neutrino flavor will not be conserved during propagation. Unlike the case
of quarks, the difference between the neutrino masses (as given by the Maki
Nakagawa-Sakata (MNS) matrix) is sufficiently small that the flavor can
noticeably change over macroscopic scales (i.e., - 180 km, KamLAND (2003)).
The effects of neutrino propagation in homogeneous density matter was
initially described in terms of an optical analogy, where neutrinos propagating
through matter forward scatter from off of the background matter inducing indices
49
of refraction for Ve, vI! and V't whose magnitude depends upon the flavor. Under
these circumstances, Ve and vJl will have different indices because the ambient
background contains unequal amounts of electrons and muons (essentially zero),
so that if the neutrinos are massive then the flavors will mix in accordance with
the mass matrix as they pass through the solar core whereas vJl and V't will have
the same values for n. Because the index of refraction acquired by the electron
neutrino behaves in a way that is similar to an additional mass term, the flavor
dependent indices can greatly affect the degree of mixing of the mass eigenstates
during neutrino propagation. This disparity between the index of refraction for Ve
and vJl (or v't) can lead to resonant enhancement or suppression of Ve, if the
neutrino has sufficient energy as it propagates through the resonance region of the
Sun.
The time evolution of the state vector in matter in the flavor basis is
governed by the equation
i.!!-(Ve(t)J =_l_(m; cos2
B+ m~ sin2
B+ A ~sin BcosB J(Ve(t)Jdt va(t) 2£ ~sinBcosB m;sin2B+m~cos2B va(t)
where the eigenvalues of the squared masses of the matrix equation for Ve and Va
are (Appendix C)
and the equation for the mixing angle in matter is
50
• 2 28 _ 1::.2
sin2
28sm M - ( )2 2'
I::. cos 28- A +1::.2 sin 28
Transforming the neutrino flavor time evolution equation into one in terms of the
mass eigenstates, (vM)[ and (vM)2 ' through a unitary transformation using
(
COS 8MU =M . 8sm M
puts the equation into a form that more clearly shows the nature of the conversion
in matter when the neutrinos propagate in a medium where the density changes
. I::. sin 28 EdAl -
-2 -2 dxm2 -m[If/M
In the adiabatic approximation, the density changes sufficiently slowly so
that the matrix in the above equation will be nearly diagonal, i.e., there will be no
mixing between the two (2) diagonal eigenstates. Provided that the off-diagonal
terms are small compared to .!. (iii; - ~2 ), the adiabatic approximation will be2
satisfied.
The amounts of Ve and Va change relative to one another, in the adiabatic
approximation. Therefore, in analogy with the vacuum oscillation equation, the
electron survival probability of an electron neutrino in matter is now given by
51
where LM = ( 4')zE is the oscillation wavelength in matterA - ~ cos 28 +~2 sin 2 28
and L is the distance from the neutrinos production point to the location of the
detector. When the neutrino passes through the critical density region, (i.e., A =
~cos28), there is resonant modification such that the resonance oscillation
wavelength is 4es = 41tE/~sin28 as long as m2 > mI.
In the level-crossing diagram (Figure 3), the straight horizontal and
diagonal lines represent the expectation values for the masses, ~2 and m~ , for the
states Ve and vI! in vacuum where the energy and mass eigenvalues for neutrinos
-2
in m~tter are given by Ek ::= P + mk and the mass eigenvalues in matter, iii;2'2p .
The behavior of ~2 and iii~ as functions of A are shown, where the ordinate is in
terms of the mass matter eigenstates and the abscissa can be taken in terms of
increasing density, p, or the resonance parameter, A. When A» ~cos28, 8M ~
1tI2 and so the heavier eigenstate V2 is almost purely Ve while the lighter eigenstate
VI is almost entirely vI!' When A =0 (i.e., for very small mixing angles) as in
vacuum, the lighter eigenstate VI is almost completely Ve while the heavier
eigenstate V2 is nearly all Va. From the above survival probability equation, it can
be seen that the nature of neutrino propagation in matter depends upon the
vacuum oscillation eigenvalues, ~2 and m; ,as well as the electron number
density and neutrino energy.
52
In the case of the Sun, the varying density between the center and the
surface causes exiting electron neutrinos to convert into other flavors because the
nature of the low-energy weak interaction is influenced by the changing effective
mass of the neutrinos in matter as the matter mass eigenstates endeavor to match
the changing density as the neutrinos propagate outward from the point of their
origin. The flavor conversion that takes place in the solar interior is due to the
change in mixing and not the change in relative phase, as in the case of vacuum
oscillations.
The large mixing angle (LMA) MSW solution offers a satisfying
explanation for the solar neutrino problem. In the case of varying density, the
adiabatic flavor conversion gradually transforms Ve into a vI! (or v1) while passing
through the resonance layer. Under these circumstances, the mass eigenstates
become instantaneous eigenstates of the Hamiltonian so that a change in mixing
takes place as the neutrino passes through the solar interior causing a certain
fraction of electron neutrinos to convert into non-electron neutrino flavors, i.e.,
ve ~ va' In the adiabatic approximation, the neutrino leaves the surface of the
Sun in a vacuum mass eigenstate so that there are no further oscillations enroute
to the Earth. Recent studies, however, have found a detectable transformation of
va ~ ve as the converted neutrinos regenerate when they pass through the
Earth's interior, known as the day-night effect [130,131].
53
3.0 Partial Degeneracy in the Solar Core
The electron degeneracy pressure and number density in the solar interior
can be obtained from the equations
5/2 (2 )Pe =CkT 3" F312 (1])
where C = 4~ (2mkYI2. The problem, however, is that since the electronh
degeneracy parameter, 11, is a function of the pressure and the temperature, i.e., 11
=11(P ,T), the equations must be solved through iteration using the two equations
[ref. 60, p. 27]:
and
(Y Z J 1 =f (dUrfJP-pRT X +-+- =- pne(p) - P4 Az 3 0 dp
where f3 = 1 - aT4/3 P is also a function of temperature and pressure, f3 = f3(P, T).
Another way of saying this is that these interrelated equations must be solved
simultaneously with respect to a particular solar model. Here, the standard solar
models (SSMs) developed by J. Christensen Dalsgaard (JCD1987)1 and J.N.
I http://www.helios.tllc.gong.noao.edu/teams/models/gong-www.14b.d.18.html (MNRAS 199(1982) 735).
54
Bahcall and M.H. Pinsonneault (BP2000)2 will be used to obtain the needed
density profiles as functions of the pressure and temperature, i.e., p =p (P, T). By
using the relation between the electron degeneracy parameter and the solar
pressure, the percent change in the electron degeneracy pressure could be arrive at
as a function of the solar radius with the help of these SSMs. The electron
degeneracy overlaps with the same region where the MSW effect occurs in the
Sun (0.1 Ro - 0.3 Ro) for various energy neutrinos. (See Figure 9.) In this study,
the total percent change in the electron number density at the solar center was
found using the ratio between the FD integrals F312 (17) and F1I2 (1]) [ref. 17, p.
97]. The maximum value of the partial electron degeneracy at the solar core
using this technique was found to be around 1.8%.
The differences in the maximum value for the electron degeneracy
between calculated values from Stix (-1.7% (Figure 6» and those performed here
(Figure 9) may be due to the fact that values for 11 are model dependent, i.e., 11 =
l1(P ,T), so the differences in the partial degeneracy of the solar interior requires
close examination when detailed comparisons between standard solar models
need to be made, because a linear approximation between various FD integrals
was used instead of calculating them individually for each solar shell.
2 http://www.sns.ias.edul-jnb/SNdataJExporUBP2000lbp2000stdmodel.dat (Astrophys. J. 555,(2001) 990).
55
The linear approximation used for the solar electron number density
(fermi3.f) introduced some error into the electron degeneracy profile that can only
be corrected by performing detailed calculations for each shell of the solar model
being considered. This may be accomplished in the future by FORTRAN
programs available in [22,23]. Neither of these programs, which calculate FD
integrals, could be easily incorporated into the program which calculated the
integrated neutrino conversion probabilities written by D. Casper [62], because
the way the I/O subroutines were structured may have entailed significant changes
to the organization and possibly the integrity of the algorithms. In the future an
entirely new procedure should be written that calls each of the routines in a clear
and consistent manner while continuously checking for errors and any possible
instabilities in the calculations during run time. The best way, however, to obtain
the most accurate electron degeneracy profile is through the implementation of a
routine during the run-time calculations of a given SSM.
In light of these considerations, the question which this paper raises is how
much does the electron degeneracy pressure influence the resonant matter
oscillations of the electron neutrinos exiting the solar core, i.e., what is the percent
difference in the total electron survival probability after passing through the
critical density regime with and without electron degeneracy? Even though the
influence of electron degeneracy on the MSW effect in the Sun amounts to only a
small correction, the importance of such effects may become increasingly relevant
as more precise neutrino experiments and solar model calculations are conducted.
56
For instance, the relativistic effects of solar electron degeneracy [63] and the
possibility of density fluctuations in the solar core [57] are now being studied
because the high degree of precision attained by neutrino experiments and SSMs
allow for such meticulous scrutiny. More detailed calculations that include solar
opacity calculations also incorporate the effects of partial electron degeneracy
[77].
In the case of high-density matter, accurate calculations of the survival
probability of electron neutrinos may shed significantly new information on the
neutrino emitting processes associated with core collapse of massive stars during
supernova (SN) explosions as well as physical properties of neutrinos. For
example, in calculating the electron neutrino survival probabilities for the thermal
stage of core collapse, accurate values of the solar neutrino oscillation parameters,
I1m;z and BIz' are needed. The importance of the MSW effect in SN explosions
arises because, in addition to the neutrino emitting thermonuclear processes
taking place in the Sun, SNe are believed to be the only other naturally occurring
phenomena where neutrinos can be measured -- assuming that the core collapse
occurs within 50 kpc. Through such astrophysical events, such as SN 1987A, a
determination of (or, strong bounds on) the absolute masses of the neutrinos
becomes possible because of the great distances between the neutrino source and
the detectors allowing for incredibly small mass differences to be determined
[64].
57
A verifiable determination of the absolute magnitude of the neutrino
masses is a question of great theoretical interest for physics, astrophysics and
cosmology. Inversely, through helioseismologicalobservations, a more accurate
density profile of the Sun may be achieved. At present, a good deal of the
calculations being done on SN neutrino fluxes treat the case when the degeneracy
parameter 11 is set to zero. Investigating the effects of electron degeneracy on SN
neutrino emission and flavor conversion may prove to be worthwhile because of
the fact that the theory of partial degeneracy is well understood, and, additionally
it is conceivable that detailed information of the effects of electron degeneracy on
the MSW effect in the case of the Sun may offer some valuable information in the
case of SNe neutrinos.
During the later stages of stellar evolution (or during supernova
explosions), the kinetic energy of the electrons in the central regions of the
matured Sun will become large enough (on the order of billions of years when it
becomes a white dwarf star) so that the magnitude of the thermal energies will
approach the rest mass of the electron, i.e., kT - mec2 and ve - c. Integrating
over the momentum space gives relativistic expression for the electron number
density
where the Fermi distribution function is given by f = (1 )/kT [65].e 1+ e e-p,
58
4.0 Neutrino-Emitting Thermonuclear Reactions
The process of nuclear energy generation taking place in the Sun's core
produces radiant energy in the form of photons which provide a radiation pressure
that counteracts the contracting gravitational force. Throughout the Sun's lifetime
these same nuclear reaction processes bring about chemical transformations that
change the Sun's structure and subsequent evolution. The energy generation of
the present Sun, however, is sustained by burning hydrogen through the proton-
proton chain and theCNO cycle where any variations in composition, temperature
and density affect the relative frequency of the various pp branches. This is one of
the principle hypotheses underlying standard solar models [66].
The first step, in the transmutation of hydrogen into helium via the pp
chain, occurs when two proton nuclei penetrate the electrostatic Coulomb barrier
and achieve nuclear fusion. The primary sequence of the pp chain, the Im1
branch, is shown in the table below.
h [59 60]Ibd fT bl 1 N Ia e uc ear reactIOn ata or PP ranc ,Nuclear reaction Qth (MeV) Qv (MeV) Time
P+ p~d+e++ve 1.192 0.250 1.4 x lOw yrs
p + d ~ 3He +Y 5.494 ----- 6sJHe + jHe~4He+2p 12.860 ----- 10° yrs
Because the first two steps must occur twice, in order for the final step in the ppl
branch to complete, the total energy liberated in the formation of a helium nucleus
is 26.732 MeV where Qth is the thermal energy delivered to the interior of the Sun
59
and Qv is the average energy lost to the Sun through neutrino emission (0.5 MeV).
In the formation of the deuterium nucleus, along with the simultaneous production
of a positron and electron neutrino, there is a sufficiently low nuclear reaction
conversion probability so the p + P reaction ultimately determines the overall rate
of solar energy generation. This is due to the fact that the reaction takes place
through the weak interaction with its characteristically small interaction cross-
section ((j oc G;). The extremely long time that it takes to create deuterium
explains the gradualness with which the Sun bums hydrogen.
In the following table for the pp2 branch of the proton-proton chain, the
neutrino emission line for the formation of lithium-7 is split because the final
product may be in either an excited state or its ground state, so that emitted
electron neutrinos appears as two distinct lines. Another important emission line
that appears in the proton-proton chain (not shown in the table) takes place
through the three particle reaction p + p + eO ~ d + Ve. However, this reaction's
rate of occurrence is only 14 % that of the p + p ~ d + e+ + Ve reaction [ref. 60, p.
48] whose average reaction time is 1012 years [ref. 60, p. 67].
h [59 60]2bd t fT bl 2 N Ia e uc ear reaction a a or pp. ranc ,Nuclear reaction Qth (MeV) Qv (MeV) Time3He + 4He~7Be + y 1.586 ----- lOt> yrs7Be + e- ~ 7Li + Ve 0.049 0.862 (0.384) 36 dys'Li + p ~ 2 4He 17.348 ----- 5 min
60
The pp3 branch begins with the same first step as the pp2 branch, i.e., the
formation of beryllium-7, but then proceeds via proton capture instead of electron
capture in the following sequence:
h 5 63bd f hT bl 3a e : Nuc ear reactIOn ata or t e PP: ranc [ 9, 0]Nuclear reaction Qth (MeV) Qv (MeV) Time
7Be +P ~ 8B +Y 0.137 ----- 100 yrs8B ~ 8Be* + e+ + Ve 7.9 7.2 0.8 s1SBe ~ 2 4He 2.995 ----- 10=TO s
The interpolated reaction rate for the pp chain is given by Epp oc pX2 T64 [ref. 67,
p. 83] where p is the mass density, X is the mass abundance of hydrogen, and T6
is the absolute temperature in units Tn = T/lOn K. According to the SSM, the
eNO, or carbon, cycle accounts for only about 1 - 2% of the energy generation in
the Sun:
I [59 60 66]br d t f h
Marks begmnmg of secondary reactIOn sequence WIth a 1/10 occurrence ratio
a e uc ear reac Ion a a or t e car on cyc e , ,Nuclear reaction Qth (MeV) Qv (MeV) Time12e + P ~ l3N +Y 1.943 ----- 1.3 x 107 yrs13N~l3e+~+e++ Ve 1.514 0.7067 7 minl3e + p ~ 14N + Y 7.551 ----- 2.7 x 1O() yrs
14N + P ~ 150 + Y 7.297 ----- 3.2 x 1cr yrs150 ~ 15N + e+ + Ve 1.754 1.00 82 sl:lN + p~ 12e + 4He 4.966 ----- 1.1 x 105 yrs160 + P ~ 17F + Y 0.600 ----- -----
17F ~ 170 + e+ + Ve 1.763 0.9994 -----lIO + P~ 14N + 4He 1.191 ----- -----
a
T bl 4 N
61
As can be seen from the primary reaction sequence, four protons are converted
into one helium nucleus with a total energy generation, Q =Qth + Qv=26.732 MeV
which is the same as that produced by the proton-proton chain. The bottleneck in
the carbon cycle is the 14N + P~ 150 + Y step since the average time required
for the transmutation of nitrogen-I4 into oxygen-I5 is over 300 million years.
The interpolated energy generation rate for the CNO cycle written as
fCNO oc pXXcNT619 [ref. 67, p. 83] where XCN as the sum of Xc and XNis used
because the mass fraction for XCN is constant while the individual carbon and
nitrogen fractions change [ref. 67. p. 81]. The pp chain dominates at temperatures
less than T = 1.5 X 107 K whereas at higher temperatures the CNO cycle takes
over and pp chain becomes unimportant since the reaction rate for the pp chain
goes as fpp oc T64 while that for the carbon cycle is fCNO oc T6
19. The Sun,
therefore, only generates about 1.6 % of its energy from the CNO cycle since Tc
= 1.57 X 107 K while the remaining 98.4% is created through the reaction
sequences associated with the proton-proton chain.
Variations in the temperature and densities in the interior of the Sun lead
to surprising differences in abundances for a range of depths, even for a single
reaction. 3He consumes itself at the Sun's core with a mean lifetime of about 106
years, yet it accumulates significantly at a depth of about RoI4, or 2 x 108 m.
Meanwhile, 4He is steadily accumulating in the central region of the Sun. For a
number of nuclear species, such as 2H, 7Be, 7Li, 8B and 8Be*, relatively short
lifetimes cause them to come into rapid equilibrium. The densities of the various
62
species do change but at sufficiently slow rates so that their abundances follow
other less rapidly changing species. Looking solely at the neutrino producing
reaction steps, we find:
[5960 68]t .T bl 5 R f d t fa e eac IOn a a or neu nno processes , ,Nuclear reaction Chain/branch!cycle Qv (MeV)a Qmax (MeV)IH(p, e+ Ve)2H pp1,pp2,pp3 0.250 0.4207Be(e-, Ve)7Li pp2 0.813 0.862(0.384)8B(e+ve)8Be* pp3 7.2 14.0613N(e+Ve)13C CNO 0.7067 1.199150 (e+ve/
5N CNO 1.00 1.73217F(e+ve)170 b CNO 0.9994 1.740IH(p e-, Ve)2H pp1 1.442 1.4423He(p, e+ve)4He pp1 -10 18.773a Qv is the average neutrino energy bThis reaction rate is negligible: 1/103
The total average energy yield per cycle in the Sun (less that due to neutrino
losses) is about 25 MeV and the total solar luminosity Lo =3.85 X 1026 W, so the
number of neutrinos produced from the hydrogen burning proton-proton chain
and the carbon cycle is Nv = Lo/<E> =(3.85 x 1026 J/s)/(4.01 X 10-12 J) =9.60 x
1037 vis. However, since two neutrinos are created for every 25 MeV produced,
63
the total number of neutrinos emitted is Ny = 1.92 X 1038 vis. The total flux of
neutrinos reaching the Earth per second per square meter is given by f =Ny/cr, so
f =Ny /4nR2 =(1.92 x 1038 vis) 14n(1.496 x 1011 m)2 =6.83 x 1014 v/m2/s.
There are also neutrinos which are formed in the rare three particle pep
reaction, p + p + e- -7 d + Ve and the highest energy neutrino emitting hep
process, 3He + p -7 4He + e+ + Ve which must also be taken into account. From
the above table of neutrino producing reactions, the neutrinos emitted with
electrons have continuous energy distributions described by Fermi's theory of
beta decay [69] while those such as the pep reaction and 7Be(e-,ve)7Li exhibit
discrete neutrino line emission spectra.
4.1 Nuclear Reaction Rates
The equilibrium reaction rate formulae for Epp and ECNO are actually not
useful for obtaining the solar neutrino spectrum; instead, all the nuclear reaction
rates for each individual reaction in the pp chain and the carbon cycle must be
used. To correctly derive the formula for the nuclear reaction rates, one should
realize that the elementary reaction process describes the collision between two
completely ionized nuclei, where the number of interactions that take place per
cubic centimeter per second can be represented as [ref. 67, p. 77]:
64
=
r = f N 1N2Vq(V)Pp(v)PND(T,v)dvo
where the number of colliding nuclei, Ni, are proportional to the density p and
their respective mass abundances Xi, i.e., Nj oc pXj. The frequency of collisions
between the first and the second nuclei is proportional to the relative velocity, v,
between them and to the effective cross section, cr(v), where cr =).,} oc l/v2 and A
is the de Broglie wavelength, A= hlmv. By comparing the thermal energy of the
nuclei in the core of the Sun with the Coulomb energy, it is clear that quantum
mechanical tunneling is needed to obtain a finite penetration probability.
A value for the thermal energy can be obtained from the equipartition
energy Eth = 3/2 kT = 1.5(1.38xlO-23 J/K)(1.57x107K) = 3.25 x 10-16 J = 2 keV.
The classical energy needed to penetrate the Coulomb barrier in the case of the
1(1.44xlO-1sm)=1.6xlO-13 J = 1 MeV. Obviously, the thermal energy of the nuclei
in the interior of the Sun is insufficient to (classically) overcome the electrostatic
barrier. The penetration probability for quantum mechanical tunneling is found to
be Pp - e-22 [ref. 70, p. P24]. Though a small number, it is significantly larger
than that obtained using a classical description, i.e., Pp _10-434 [ref. 71, p.149].
The equation that describes the penetration probability with quantum
mechanical tunneling is given by [ref. 67, p. 77]:
65
This equation shows that the penetration probability drops for collisions with high
charges and for low velocities:
[T]he penetration probability, Pp, rapidly decreases with decreasing
particle energy. On the other hand, as the energy increases above
the thermal average the number of particles of a given energy
rapidly decreases, according to Maxwell's Law. Clearly then, the
main contribution to nuclear processes will arise from particles in
an intermediate range, such as EStellar= 20 kev. [ref. 67., p. 74]
Because both the penetration probability and the collision frequency depend
sensitively on the relative velocities between the particles, integration over the
frequency distribution of velocities, D(T,v), must be included. The Maxwellian
distribution, D(T,v) oc vZr 312exp[-(1I2)HAI,z vZ/kT] [ref. 67, p. 78] can be used
since the pressures are low enough that one would not expect any degeneracy
except at the very center of the Sun. In the above equation, the reduced atomic
mass is Al,2 = (AI + Az)/AIAz, andH stands for hydrogen. Nuclear penetration
does not ensure that a nuclear reaction will take place. PN, the probability of
nuclear reaction, depends very sensitively on the particular type of reaction so it is
a important factor in determining the final reaction rate. It is, however, the
velocity distribution on temperature that makes the reaction rates so sensitive to
temperature. The evaluation of the integral,
66
r = fN1Nzvq(v)Pp(v)PND(T,v)dv, is simplified because a narrow range in velocity
supplies very nearly the complete value so that the main contribution to the
nuclear processes comes from particles at intermediate energy values.
Energy generation per unit mass, t, is defined in the equation
dUdm =t - tv - T(dS/dt)
where dUdm is the change in luminosity in Lagrangian coordinates, i.e., the
energy passing through a spherical mass shell, s is the specific entropy, t
symbolizes the nuclear sources per unit mass, tv the energy losses due to neutrino
emission and the T(dS/dt) term represents any heating or cooling that may take
place in the star and affect its temperature. Because the Sun is nearly in thermal
equilibrium, the change in the specific entropy should be negligible, so the energy
generation equation can be simplified to dUdm = t, where the neutrino energy
losses have been eliminated, and the source term, t, depends upon the density,
temperature and mass abundances of the various nuclear species, t =t (p, T, Xi)
[ref. 71, pp. 22-23].
Given that the nuclear reactions take place in the central region of the Sun
where the mean free path of a photon is so small that the temperature where the
photon is emitted is virtually the same as that where it is absorbed, then the
assumption of thermal equilibrium in the core is a satisfactory approximation. In
this approximation, the temperature gradient can be expressed as
dT/dm =-3KL/256nzoR4T3 where K is the Rosseland mean opacity [ref. 60, p.
21].
67
Seeing as the hottest region of the Sun is in its central core, complete
ionization can be assumed for the reactions thus allowing the equation for the
electron densities to be simply written as ne =pNA(l + X)/2 where NAis
Avogadro's number [ref. 60, p. 27]. (See Figure 10.)
Partial electron degeneracy occurs deep in the Sun's interior,
where the density is high [...T]he correction becomes significant
at P :::::: 1014 Pa, corresponding to r:::::: ro/2, and reaches about 1.7% at
the center" [ref. 60, pp. 26-7].
(See Figure 6.) Because of the complexities associated with the particle-particle
interactions that occur in the core, tables of the density and opacity determined
from numerical computations are commonly used. Nevertheless, a useful
expression for the opacities called the Kramers opacity for free-free transitions
[ref. 71, p. 138],
Kff =3.8 X 1022 (l + X)[(X + Y) + Z]p/T3.5
is often used where X is the mass fraction of hydrogen and Y is that for helium,
and Z is for all other heavier elements. Here, the term 1 + X is included because
Kramers opacities are found to be proportional to the electron density. (Often a
correction due to quantum mechanical effects is also included called the Gaunt
factor, so Kff - gpT3.5.) The important point here is that because the nuclear
reaction rates of the various nuclear species depend on density, temperature and
composition, the rates are then also dependent on the particular solar model being
used. It, therefore, becomes vital that the assumptions and approximations made
68
in the respective solar models are actually physically allowable. The accuracy of
the nuclear reaction rates are critically important for predicting with sufficient
precision the neutrino fluxes emitted from the Sun. The cross section factors,
SeE), have been particularly scrutinized as a source of inaccuracy.
The modeling of high precision data from helioseismology demands
significant accuracy in the equation of state (EOS) which allows for a check on
the input physics describing the stellar interior and envelope [72]. As mentioned
in the previous section, the number density for relativistic electrons can be written
as [73]
where
The Los Alamos Opacity Code EOS is based on the Saha equation1 which
includes degeneracy. Detailed information describing the underlying atomic and
radiative processes relevant to calculating the solar opacity can be found in [74].
1 The Saha equation gives the relationship between free particles and those bound in atoms. Morespecifically, it is a formula describing the thermal equilibrium of a gas of electrons and ions interms of the change in temperature. It gives us the relationship between the number of ionizedatoms of a certain species and the number of neutrals. In the case of the Sun, the central numberdensities are so large (6.4x1025/cc) that the electrons there are effectively kicked out of the atomthrough pressure ionization, i.e., r = l/nl13
- 2.5xlO'9 cm which is smaller than the Bohr radius.See [ref. 17, pp. 29-36] for more details on the Saha equation; also, see [52] for information on thederivation of the Saha equation in the case of a two-temperature plasma.
69
In partial summary, it is found that the rate at which a nuclear reaction
takes place depends on the relative velocity, v = IVI - v21 of the reacting nuclei,
the distribution of the nuclei in velocity space, D(T,v) and the cross-section, cr(v),
which is the probability that such a nuclear reaction will occur at a particular flux
density. Because the stellar interior can be well approximated by the condition of
local thermal equilibrium, the velocity distribution can be represented using a
Maxwell-Boltzmann distribution, i.e., f(v) oc exp(-mv2/kT) with only a small
percentage error at the solar center.
4.2 Cross Sections for Non-Resonant Reactions
Resonant reaction rates in the interior of the Sun are relatively rare so that
only non-resonant nuclear reactions are relevant when studying solar energy
generation in the present Sun. The cross-section for non-resonant reactions is
determined through a combination of quantum mechanical theory and nuclear
reaction experiments. The overall cross-section for non-resonant reaction can be
written as [ref. 60, p. 36]:
cr(E) = (1/E)S(E)exp[-(m/2E)1I2(Zi Zj e21t1coh)]
The cross-section factor, also known as the astrophysical cross-section, SeE), is
found from nuclear experiments [75]. But since the energy range of interest (-20
keY) is significantly below the lowest energies attainable in the laboratory, values
70
must be obtained through extrapolation. Because the cross-section is proportional
to the square of the de Broglie wavelength, where)..,z =h2l2mE, the lIE factor in
the above equation makes sense. As the wavefunction for a particle that tunnels
through a barrier is always exponential (due to the requirements needed to match
the boundary conditions at the electrostatic barrier), the exponential term in the
above equation for the cross-section is also an acceptable factor. Just as the
equations describing quantum mechanical tunneling contain a negative
exponential, so it makes sense that the probability of nuclear penetration would
also include such an exponentially decreasing function. For non-resonant
reactions, the cross-section factor, SeE), can be taken out of the integral because
as a slowly varying function of energy is it nearly constant over small changes in
energy.
The combination of the Maxwell-Boltzmann distribution factor,
exp(-E/kT), and the nuclear penetration factor, exp[-(ml2E)1I2 (Zi Zj e27t1coh)],
produces a sharply peaked function known as the "Gamow peak." (See Figure
13.) Setting the term in the exponent of the penetration factor (less E) equal to b,
which represents the barrier, an energy where the Gamow peak is a maximum can
be derived where Emax =(bkT/2)2/3. Approximating the Gamow peak, exp[ -E/kT
- b/(E)112] , with a Gaussian and taking the constant term So outside, allows for the
integral to be evaluated analytically, so that [ref. 60, p. 36]:
cij{T) =4 S(Emax) (2/3m)1I2 (bl2)113 exp[- 3(bl2)213/(kT)1I3]/(kTl3.
71
This approximation shows the characteristic temperature dependence of T I/3 in
the exponent and the T 2/3 term in the multiplicand for non-resonant reaction rates.
The additional terms which appear in the energy generation formula, such as
(1 +0.123T91/3 +1.09Tl/3 +0.938T9), are corrections that arise due to the non
Gaussian shape of the true Gamow peak. More details on the derivation of the
nuclear energy generation rate are given in Appendix B.
In summary, the most important nuclear reactions taking place in the
interior of the present Sun have been described. Information concerning solar
neutrino emission was examined where it was found that the total solar neutrino
rate of production is about 1.9 x 1038 vIs and the total number of neutrinos that the
Earth receives per second is roughly 68 billion per square centimeter. Nuclei with
intermediate thermal energy (- 20 keV) provide the primary nuclear reactants in
the core of the Sun due to two competing processes: 1) a Maxwellian velocity
distribution probability, and 2) a quantum mechanical tunneling probability which
gives rise to a non-Gaussian Gamow peak. In the energy generation analysis, the
energy loss due to neutrino emission, Ev, and those attributed to local heating and
cooling, T(oslot), are neglected. The Ev are neglected because once they leave the
solar interior within a matter of seconds they play no role in thermal heating, and
the T(oslot) term is ignored because the short path lengths in the solar core
ensure that the particles find themselves in local thermal equilibrium.
72
5.0 Standard Solar Models
Due to complexities associated with radial composition inhomogeneities,
thermonuclear reaction chains, opacities and convective energy transport, detailed
numerical stellar modeling becomes inescapable for any thorough investigation of
the solar interior, especially when fairly small effects such as those due to the
influence of electron degeneracy on the adiabatic flavor conversion of electron
neutrinos are to be extracted. Yet, even for mature stellar structure codes that
have evolved over the decades, physical phenomena associated with rotation,
magnetic fields, stellar winds, coronal mass ejecta, general relativistic effects and
other complications are generally ignored. Standard solar models treat the Sun as
a spherically symmetric, non-rotating, luminous plasma whose chemical
composition is radially inhomogeneous and exists in steady state equilibrium.
Such models describe the Sun in terms of mechanical, nuclear and
chemical equations. From astronomical observations and theoretical calculations
for stars forming in the galaxy, accurate values for the chemical composition of
typical population I stars are obtained, i.e., X =0.71, Y =0.27 and Z =0.02.
These mass fractions for hydrogen, helium and heavier nuclei are introduced as
starting values into the stellar formation part of the code for the primordial zero
age main sequence (ZAMS) Sun (t = 0) which are then allowed to evolve to the
present epoch (t :::: 4.6 X 109 yrs).
73
5.1 Equations of Stellar Structure and Evolution
The system of equations which govern the physical structure and
processes of this evolved, steady-state main sequence Sun are given by five (5)
coupled differential equations, such as that for hydrostatic equilibrium:
dP GM(r)p(r)- =----,-----dr r 2
where P is the pressure, M(r) and p(r) are the mass and density for a given shell
radius, r. This equation shows that for a star in hydrostatic equilibrium the
inward pull of gravity is exactly balanced by the outward pressure of each discrete
shell in this "onion skin" solar model. Conservation of energy and energy
transport equations for radiation and convection are also required along with the
appropriate equations for chemical composition and nuclear energy generation.
The equation relating the mass of the Sun to its radius is given by the mass
continuity equation:
dM(r) =4m 2p(r).dr
For a non-barotropic equation of state (i.e., not dependent on pressure alone), the
pressure is related to the density and the temperature as in
P(p,T) =pkBT (l+D)+ aT4
Jl111 H 3
74
where kB is the Boltzmann constant, a, the radiation constant, Il, the mean
molecular weight, mH, the mass of a hydrogen atom and, T, the temperature. The
first term on the right-hand side of the equation is the thermal pressure and the
second term, the radiation pressure and D includes corrections due to electron
degeneracy pressure and electrostatic interactions [ref. 59, p. 49] where the
electron degeneracy can be represented as a function of FD integrals. The mean
molecular weight is represented by the equation
Jl =(_1+_1J-1
Jlion Jlelectron
1 4X +Y 1 2X +Ywhere -- :::: and :::: when Z « X.
Jlion 4 Jlelectron 2
The equations describing the radiative and convective transport are
and
(dT) =(l-!JT dP =-\7ad(PTG~(r))dr conv Y Pdr Pr
y-1 Cwhere \7 ad =-- and y =-f.. , the ratio of the specific heat at constant
y Cv
pressure divided by that at constant volume. The value for the adiabatic gradient,
\7 ad ' depends on the various ionization processes taking place in the solar
interior. The opacity, K, depends on the temperature, pressure and composition at
a given radius, i.e., K =K(p, T, XD. While there are no simple analytic
75
expressions that completely describe K (most stellar models obtain opacities from
numerical calculations or tables), there are some useful approximations for the
most important atomic processes 1) the Kramers opacity arising from free-free
absorption [ref. 76, p. 60]:
2) the electron scattering opacity due to radiative scattering from free electrons
Kes :::: 0.2(1 + X)cm 2/ g ,
and 3) the bound-free opacity from radiative scattering from ionized atoms
Calculations of the radiative opacity often include the effects of partial
degeneracy on free-free absorption and photoionization cross-sections as well as
corrections to the elastic scattering cross sections. Most modelers of the solar
interior use opacity tables from numerically computed values, such as the Los
Alamos Opacity Library. Advances have been made to improve on the stellar
opacity calculations for the solar interior extending from the Los Alamos Opacity
Library [77] to OPAL95 [78].
The last of the coupled, nonlinear partial differential equations that make
up the main equations of stellar structure follows from the definition of luminosity
dL(r) 4 2 ()--= mprcdr
76
where the nuclear energy generated, £ =£(p, T, Xi), depends on the relevant
nuclear reactions at a given temperature, density and composition and where the
particular form of £ determines the variety and location of the energy producing
mechanisms. Most of the energy (98.4%) produced by the Sun is obtained from
the pp chain where
_ 2.4x104pX 2 -3.380IT,j/3
C pp - 2/3 eT9
while the remaining 1.6% is attributed to the carbon, or eNO, cycle
_ 4.4x1025
pXZ -15.228IT,j/3CCNO - 2/3 e
T9
These can be approximated by power law relations to show that Cpp oc pT 4 and
CCNO oc pT 15-
18 [ref. 76, p. 63]. One of the key features about these equations is
that they are acutely sensitive to changes in temperature. For a specific example,
in terms of flux, the decay of boron-8 - a critical neutrino generating reaction - is
related to temperature by
Such delicate sensitivity on the central temperature can often lead to significant
errors in developing accurate solar models. The neutrino flux for the pp chain
reaction is about 6 x 1010 cm2/s, whereas for ¢J(8B) the value drops to about
5 X 106 cm2/s. (See Table 10.)
Given the constitutive equations, i.e., £ = £(p, T), K = K(p, T), and the
equation of state, P =pep, T), the equations of stellar structure (the equation of
77
hydrostatic equilibrium, mass continuity, radiative or the convective temperature
gradient and luminosity gradient) can be integrated to obtain the equilibrium
structure of the Sun.
The above differential equations governing stellar structure are often
recast into Lagrangian form using the assumption that the total mass of the Sun
remains constant [ref. 71, p. 64]:
aram
1
ap Gm 1 ar2
=--------am 4m 4 4m 2 at 2
aL aT 0 ap-=£ -£ -c -+--am n V P at p at
aTam
The equation connecting the differential equations in Eulerian form to those in
L . f' ala. b' 'd dagranglan orm IS - = 2 ,I.e., y treatmg m as an m epen entam 4m par
variable and r as a dependent variable. Notice that the first four equations are in
terms of the partial differential mass, sometimes called the "spatial" equations
whereas the equation relating the chemical composition is a partial differential of
the time. The second of the above equations would not include the term
78
1 ar 2
'f' 'd 'l'b ' I hi" d'- --2-2 1 It were m stea y state eqUl 1 num. n t e ummos1ty gra lent4nr at
equation, En stands for the nuclear energy generation per unit mass, Ev, the energy
loss due to neutrino emission, c5 = -(aIn p) and V = din T in the thermalalnT p dlnP
gradient equation. Likewise, the last three terms on the right hand side of the
1 " , c aT c5 ap 11' 1 d d 'ummos1tyequatIOn, - Cv - p - +--, are usua y not mc u e mat p at
calculations in the standard solar model. They are shown to illustrate some of the
approximations that are often made for such calculations. Some relatively recent
models include equations that regulate the mixing in the convective region, e,g.,
ax i = 1 (mI2
ax i 1 +am2 (x. - x. )+ am! (x. - x. )Jat m
2- m! at m at 12 1 at 11 1
ml
where 1m is the mixing length obtained from mixing length theory.
Given this full set of stellar structure equations with the independent
variables m and t, the physically relevant solution can be determined as long as
suitable boundary conditions and initial values are provided. Such a system of
partial differential equations must be solved numerically as a boundary value
problem because there are no analytical solutions to such an involved system of
nonlinear, coupled differential equations. By using four (4) first order differential
equations, three (3) auxiliary equations (i.e., E, K, P), in terms of seven (7)
variables (i.e., p, T, L, P, K, E, and rem)), along with four (4) boundary conditions
(two at the surface: m = Mo, P ::::: T ::::: 0, and two at the center: m = 0, and r = L =
79
0), the resultant system is well defined and leads to unambiguous properties once
the total mass, initial radius and initial composition are given.
5.2 Numerical Methods for Solar Modeling
Problems arise when the calculations are naIvely attempted by starting
either at the center and integrating outwards, or beginning at the surface and
integrating inwards because, if any of the variables, say P, goes to zero before any
of the others while the integrations are being performed, the calculations become
unstable and lead to erroneous results. The shooting or integration method solves
this problem by integrating outward from the center while simultaneously
integrating inwards from the surface where the two results meet smoothly at some
intermediate regime, such as at the interface between the radiative and the
convective zones [ref. 71, p. 77]. The calculations are matched at the so-called
"fitting point" by incrementally varying the trial solutions at the solar center and
surface until a smooth fit is obtained. One of the disadvantages of the integration
method is that it cannot handle regimes of nonlinearity and rapidly varying
functions that are needed to describe later stages of stellar evolution.
The integration method is ideal for stars with homogeneous composition
gradients that are on the main sequence, i.e., a ZAMS star. The above
approximate boundary conditions at the surface arise because of the complexities
associated with the solar atmosphere, e.g., if T = 0 at the surface, there would be
80
no radiation. Additionally, because of the existence of a hot corona, the condition
of hydrostatic equilibrium cannot be maintained.
In the case of nonhomogeneous compositions, as for the Sun, the Henyey
iteration method can be successfully used where the solar interior is divided up
into a number of mass shells with appropriate boundary conditions so that the
structure equations can be used to determine the various relations at each of the
discrete mesh points which are connected by a series expansion between the two
shells using a simultaneous multidimensional Newton-Raphson iteration method
[79]. The Henyey iteration method is a very stable way to perform the
calculations to obtain relatively accurate stellar structure information without
small errors propagating out of control, i.e., it is consistently stable and reliable
[ref. 71, pp. 78-83]. One of the shortcomings of the Henyey method is that, due
to the difficulty associated with splicing together linear approximations,
significant inaccuracies can arise -- especially in the case of thin burning shells.
Another of the limitations of the Henyey iteration method is that it is only
good if an approximate solution to the stellar structure equations is already
available, so that, given a particular trial solution, the system of equations is
improved in each iteration until the desired degree of accuracy is reached. For
systems where there are no available approximate solutions, such as for the
evolution of high mass stars, methods using a combination of the integration and
the Henyey methods have been developed and are known as multiple fitting point
methods. The multiple fitting point method is a more general method that
81
includes the strengths of the integration method (allowing for access to already
optimized numerical integration techniques for differential equations) and the
strengths of the Henyey method (providing the requisite stability so that advanced
stages of stellar evolution can also be studied in sufficient detail). The way the
method combines the best features of the other two numerical integration methods
is by performing actual integrations between the shells [80].
5.3 Standard Solar Models
John Bahcall and company have been deeply involved in improving the
standard solar model for over thirty-five years. Recognizing the importance of
developing sufficiently reliable models to be able to study the weak interactions in
the Sun, Bahcall et al. have tenaciously brought to bear a wide range of physical
features needed to better understand the underlying solar physics which lead to
highly accurate standard solar models [59]. Hundreds of improvements were
made to the input parameters over the decades along with appropriate
modifications to account for the best available physics. This is why they are
called "standard" models - they include standard accepted physics as opposed to
non-standard models which make some non physical, or not yet accepted,
assumptions in order to obtain "improved" fits for their data. Bahcall had early
on realized the crucial importance of identifying and reducing the uncertainties,
such as those associated with 1) the predicted neutrino fluxes, 2) neutrino
82
production rates, 3) nuclear cross sections, 4) the equation of state, 5) solar
luminosity, 6) elemental abundances, 7) radiative opacity and 8) the solar age, in
attempting to explain the solar neutrino problem in terms of the MSW effect.
Such calculations require a series of models, one for each of the various
evolutionary sequences - often about half a dozen - which are then iterated until
the calculated luminosity and radius produce a difference with the observed
values of less than one part in one hundred thousand. The initial model of the
primordial Sun is represented as chemically homogenous. The change in the
various chemical isotopic abundances is obtained from the various nuclear
reactions where more recent computations now include diffusion effects for some
elements, such as for helium. It turns out that determining acceptable values for
solar interior parameters needed to study solar neutrino physics do not require
very accurate description of the Sun's atmosphere. This is fortunate because the
physics associated with describing the solar atmosphere are inherently difficult
because of the complexities associated with instabilities and the outer-lying
corona.
One crucial advantage such solar modelers have is by comparing their
numerical calculations with those obtained from helioseismology, such as the
pressure frequency oscillation modes, known as p-modes, from such projects as
GONG (global oscillation network group) and SORO (Solar and Reliospheric
Observatory). These p-mode oscillations offer a means to obtain very accurate
values for the temperature, density and composition distribution inside of the Sun.
83
These frequency oscillations are acquired from observations of small motions that
periodically occur on the solar surface. l Some of these oscillation measurements
are among the most precisely known astrophysical quantities rivaling even those
obtained from some of the best terrestrial experiments [ref. 59, p. 109].
In conjunction with solar neutrino experimental data, greatly improved and more
reliable calculations and models have been developed. Because of such sustained
advancements in the field of solar modeling over the past three decades, attention
can now be focused on establishing more accurately 1) the distribution of solar
neutrino production, 2) the shape of the neutrino energy spectra, 3) neutrino
absorption cross sections as a function of energy, and 4) the Sun's electron
density profile, etc.
Some of the approximations [82] had made in their standard solar model
include neglecting radial pulsations and pressure corrections arising from the
Sun's rotation and magnetic field. Such approximations are entirely acceptable
because of the extreme accuracy associated with assuming hydrostatic
equilibrium. Acoustic and gravity waves are ignored in the energy transport
while the Rosseland mean opacity is employed to describe photon diffusion in the
radiative zone. In unstable regions of the convective zone, the adiabatic gradient
is used to describe the convective gas using mixing length theory, but not near the
solar surface [ref. 59, p. 86].
1 More specifically, solar oscillations are found from the velocity shifts in the solar surfaceabsorption lines. See the principal paper describing the discovery of the Sun's five (5) minuteoscillations [81].
84
Owing to the critical importance of errors that may enter into the nuclear
energy generation calculations, corrections due to gravitational expansion and
variations in equilibrium produced by nuclear burning are incorporated.
Modifications that include short-lived events, sudden mixing and accumulation of
matter due to hypothetical black holes, however, are not used. More recent
numerical calculations in [83] include novel precision calculations of the electron
density profile of the Sun. These recent modifications to the standard solar model
also take into account possible interaction effects which may be attributable to
hypothetical sterile neutrinos. (See Figure 15.)
In the solar model described in [82], the most important parameters which
are entered as input parameters are the chemical abundances, the radiative opacity
in terms of the Rosseland mean opacity, the equation of state and the nuclear
reaction rates. It was found that one of the most critical input parameters in the
solar model was the initial ratio of all of the elements heavier than helium to that
of hydrogen, i.e., ZJX. This sensitivity of the metallicity to the hydrogen
abundance follows from the fact that neutrino fluxes and opacities are closely
connected and the fact that opacities are strongly influenced by the heavy element
abundance, Z. The equation of state, which relates the pressure, temperature and
density, also incorporates the effects due to radiation pressure, electrostatic
screening interactions and electron degeneracy.
The usual procedure in obtaining the solar model requires guessing the
initial parameters, then stepping through the model as a function of time, where
85
the Sun's evolution is represented by a series of difference equations. Once the
iteration process gives the characteristic values for the present Sun, a close
comparison with the measured values determines the sought for solar model.
More specifically, the original homogeneous hydrogen composition, X, is
presumed along with an entropy-like variable, S, where the output from the
iterations in X and S are performed. The subsequent output gives the mass
fractions for hydrogen, helium, the associated heavy elements and a complete list
of the relevant physical variables in the solar interior as well as acoustic
oscillation frequencies and neutrino fluxes.
The initial helium abundances are obtained through the process of iteration
using as input the ratio Z/X and the constraint X + Y + Z =1.0. The values for
the initial He abundances are found to be in agreement with bounds obtained from
cosmology, present-day helium abundances in the interstellar medium of the
Milky Way galaxy as well as the initial abundance of the Sun, all within a few
percent [ref. 59, pp. 103-4].
Thus, standard solar models are the final result of a sequence of models
beginning with a homogeneous zero age main sequence (ZAMS) star, followed by
a number of succeeding evolutionary models which allow for the local
compositional changes brought about through various nuclear reactions. Some of
the changes that take place in the calculations which simulate the evolution from
the primordial to the present Sun include a 41 % and a 3% increase in luminosity
and temperature, respectively, during the period the Sun has been on the main
86
sequence, i.e., - 4.55 x 109 years. The neutrino flux from the boron-8 decay was
found to have increased by a factor of 41 since the Sun first became a main
sequence star. The luminosity boundary conditions were found to have a
noticeably large effect on the neutrino fluxes. This makes sense, however, since
they are both dependent on the thermonuclear reactions taking place deep with the
solar core. Recall, L =4nr 2 p(c +T ~~) where c represents the nuclear energy
generation per unit mass which is very sensitive to the solar central temperature.
Because of the sensitivity of the luminosity and the neutrino fluxes on the nuclear
reactions, i.e., <!>v = <!>v(L(E)), the neutrino fluxes provide a useful way to determine
the branching ratios of the competing pp chain reactions. Inversely, accurately
measuring the spectra of neutrino fluxes ought to provide a good diagnostic of the
solarinterior [ref. 59, p. 88].
It was shown in [82] and later in [83] that given the total mass, the total
luminosity and radius of the Sun (beginning with the initial guesses for X and S),
a surprisingly accurate description of the present Sun, or standard solar model,
could be obtained [84]. From these studies, it was found that the percent of the
total luminosity from the pp chain alone should be 98.4% while that for the
carbon cycle was 1.6% where 95% of the total luminosity came from within RoI5.
Out of this, the neutrino luminosity was found to be 2.3% that of the photon
luminosity and the pp chain was shown to terminate in the 3He_3He reaction
85.5% of the time whereas the other 14.5 % terminated in the 3He-a reaction.
87
6.0 Solar Neutrinos and Neutrino Experiments
Some of our best information concerning solar neutrinos comes from
standard solar models. The various neutrino energy spectra obtained from the
iterated solar models furnishes critical details for properly investigating numerous
physical details of the Sun, such as those relating to the MSW effect. Entering
data from neutrino-producing nuclear reactions allows neutrino energy spectra
and fluxes to be determined. Early work by Bahcall, Fowler, Iben and Sears
obtained valuable information about solar neutrino fluxes [85]. In particular,
calculated neutrino energy spectra of 8B, 7Be, pp, and hep reactions have supplied
useful numerical data concerning neutrino energy production as a function of
solar radius and temperature for most of the relevant neutrino fluxes. (See Figure
17.) Of the eight (8) main neutrino producing nuclear reactions and decays (pp,
7Be, 8B, hep, pep, 150 , 13N and 17F), the rare 8B decays are presently of the most
interest because these electron neutrinos have maximum energies above the
resonant energy. On-going neutrino experiments (such as SNO and SK) are
especially sensitive to the high-energy end of the neutrino spectra due to larger
interaction cross sections of their detectors. This can be better appreciated by
directly comparing the electron-electron neutrino scattering cross sections.1
1 In quantum field theoretic calculations, it is found that, for low energies,
G 2 so-(vee- ~ e-ve) =_F_. The total (low-energy) scattering cross-section for antineutrinos
7[
and electrons is 1I3rd that for neutrinos. See [ref. 61, pp. 162-3] for an outline of the derivationfor the integrated cross-sections.
88
Table 6: Electron-electron neutrino cross-sections, crve [59]-
ReactionlDecay E:mx (MeV) Cross-section (10-40 cm2)
liB decay 14.06 608{Be decay 0.384 59.3pp 0.420 11.6hep 18.77 884
The three continuous neutrino spectra 8B, pp and hep, have fluxes that are roughly
proportional to the squares of their respective energies, i.e., rjJ(Ev ) oc E~ and
average cross-sections that are directly proportional to the integrated flux. As can
be seen from the above table, the cross-sections increase as a function of energy.
On the other hand, because the pp chain accounts for about 99% of the total
neutrinos emitted with energies of 0.42 MeV and below, the gallium experiments
become the primary means for their detection. (See Figure 18.) Comparing the
calculated fluxes in the following table shows why neutrinos from the hep
reactions are difficult to measure.
Table 7: Calculated neutrino fluxes, <Pv [86]Neutrino Energy (MeV) Neutrino Flux (101) cm-2 S-l)
Sourcepp ~0.42 59400 ± 600pep 1.44 139 ±1.4hep ~ 18.8 =0.0021{Be 0.86(90%), 0.38(10%) 4800 ± 430liB ~ 15 5 5+0.98
• -0.72
uN ~ 1.20 605+115-79
1:l0~ 1.70 532+117
-80
89
The flux for hep neutrinos (i.e., from 3He + p ~ He + e+ + ve) is around three
orders of magnitude below that of 8B. The estimated uncertainties for each of the
above fluxes vary widely. For the pp reaction the flux is known to within 1%,
whereas for beryllium-7, boron-8 and hep they rise significantly: 8%, 18% and
unknown, respectively. (Also, see Figure 19.)
In the near future, low energy neutrinos from 7Be decays will be
specifically investigated through electron scattering using 300 tons of liquid
scintillator by Borexino (Gran Sasso, Italy) with 1000 times the 8B flux of either
SuperK (SK) or SNO with an uncertainty of less than 10% [86]. The neutrino
flux and neutrino spectra arise from nuclear reactions and decays in the region of
the solar core where, for example, 8B neutrinos are formed relatively close to the
core whereas those from the 7Be, hep and pp reactions are formed further away,
such that the maximum fraction of 8B, 7Be, pp, and hep neutrinos are produced
around 0.05Ra, 0.06Ra, O.IRa and O.13Ro, respectively. (See Figure 17.)
The above reactions also cover a broad range of temperatures. The
neutrino flux from the 8B decay is the most sensitive to the solar central
temperature:
<jJ(SB) DC TclS-ZO .
This range shows that the boron-8 neutrino flux is only an approximation because
the calculated temperature dependence relies upon the how much influence each
calculated data point -- obtained from slightly different solar models -- is given in
the fit where each such point comes from a slightly different solar model [87].
90
(See Figure 19.) It is this extreme sensitivity to the central temperature of the Sun
that accounts for much of the uncertainty in the neutrino flux from the decay of
8B.
In the case of 7Be, the calculated neutrino flux is directly proportional to
the central temperature to the eighth power, so
rfJCBe) oc Tc8
whereas for the pp reaction the neutrino flux actually falls for increasing
temperature:
The neutrino flux from the pp reaction decreases with increasing central
temperature because the reactions can terminate via the 3He-a reaction pathway
instead of through 3He_3He, thereby producing only half as many neutrinos.
The neutrino flux from the hep reaction is found to have a significant amount of
spread obtained for the various solar models, so the temperature dependence
spans a range from T} to Tc6
• (See Figure 19.)
An important distinction between the pp (and pep) and the 7Be (and 8B)
reaction is that, as the initiating reaction(s), the pp is largely independent of the
SSM whereas the electron neutrinos emitted during 8B decay are strongly
dependent on the details of the SSM. This is primarily because the ~+ decay of 8B
is the second step in the pp3 branch in addition to being exceedingly sensitive to
temperature. As shown in the above table, the eNO cycle also makes a
contribution to the neutrino flux from the ~+ decay of 13N, and 150 and 17F (not
shown). Borexino should be able to probe the domains of both astronomy and
91
astrophysics through the connection made by the 7Be step in the pp chain because
of its low energy threshold.
6.1 Solar Neutrino Experiments
Since the pioneering days of Raymond Davis, Jr. and associates - who
used Ve capture in chlorine -- an extensive variety of neutrino experiments have
been proposed using accelerators [88], nuclear reactors, radiochemical reactions
in gallium and thallium, electron recoil measurements in Cerenkov water
detectors, and heavy water deuteron reactions. Of all the solar neutrino
experiments proposed, on-going, or completed, Super-Kamiokande (SK) and the
Sudbury Neutrino Observatory (SNO) provide statistically the largest amount of
experimental data dealing with neutrinos emitted in the f3+ decay of 8B. The
relatively low neutrino flux of this decay is compensated by its relatively large
reaction cross section. Most of the other neutrino experiments are better suited
for studying neutrinos from other reactions and decays even though they also
provide important information about electron neutrinos emitted in the boron-8
decay. For example, because of the low energy threshold in the
7lGa +v e ---771 Ge + e- reaction (Eth = 0.233 MeV), the gallium experiments SAGE
[89] (Soviet-American Gallium Experiment) and GALLEX [90] are ideal for
measuring solar neutrinos created in the pp chain. The solar neutrino spectrum in
92
Figure 18 shows that the gallium detectors cover the widest range of energies at
the price of statistically reduced sensitivity to higher energy neutrinos. In the
SAGE experiment, the global best fit for the neutrino capture rate was 70.8~;:;~;:~
SNU, while Bahcall & Company's Standard Solar Model [83] predicted a capture
rate of 129~~ SNU where 69.7 SNU are attributed to the pp reaction, 32.4 SNU to
7Be neutrinos, and 12.1 SNU to the decay of 8B. The ratio of the measured
number of electron neutrinos captured to that predicted by the SSM is 0.549. In
the GALLEX experiment, the combined result for GALLEX I-IV is
77.5 ± 6.2~~·.~ SNU with a flux ratio of 0.601.
The Homestake chlorine experiment (Lead, South Dakota), using the
neutrino capture reaction 37 Cl +ve --?37Ar + e- , was originally conceived to
directly confirm that the Sun is powered by thermonuclear reactions through the
pp chain and the CNO cycle [92]. By 1968, initial results had already shown
discrepancies with the accepted standard solar models [93]. The fundamental
question raised at the time was whether it was an astronomical or a physical
problem, i.e., whether the astrophysical description of solar evolution and
structure was at fault or the underlying physics describing neutrinos was not
completely understood. Due to the fact that measurements of the nuclear cross
sections in the case of the Sun require significant extrapolation to low energies
from high energy laboratory results, a great deal of work was done to improve
93
upon the experimental nuclear physics [94]. During the same period, the SSMs
and the neutrino experiments likewise developed significantly.
A search ensued to find alternative radiochemical reactions that could
measure lower energy neutrinos because, with a neutrino detection threshold
energy of 0.817 MeV, the chlorine experiment could not measure any of the
neutrinos emitted from the primary pp neutrino generating nuclear reaction since
Eth :5 0.42 MeV. In "Solar Neutrinos: A Scientific Puzzle"[95], Bahcall and
Davis identified the gallium reaction 71Ga(ve, e-)71Ge because it had a
sufficiently low energy threshold (0.233 MeV) along with an acceptable cross
section and an intermediary with a reasonable half life (11.4 days) to capture
neutrinos created in the pp reaction. The problem however was that gallium was
not cheap and the detection process was difficult to perform. By the 1990s, these
efforts evolved into SAGE (c.1990, Baksan, Russia) and GALLEX (c. 1991)
whose successor is now known as GNO [96] (c. 1998, Gallium Neutrino
Observatory in Gran Sasso, Italy). The results from SAGE and GALLEX
confirmed that the proton-proton nuclear reaction is the primary reaction which
powers the Sun. Analysis of global neutrino data obtained an upper limit of 7.3%
for the fraction of energy produced by the eNO cycle in the Sun [97].
Kamiokande I and Kamiokande II, which use water Cerenkov detectors,
found 8B/SSM flux ratios of 0.46 ± 0.13 ± 0.08 and 0.46 ± 0.05 ± 0.06,
respectively [98]. Because of the success of the Kamiokande experiments, Super
kamiokande [99] (SK) was proposed in 1990. The primary physics goal of SK
94
was to identify any baryon number violating processes, i.e., proton decay, in an
effort to test grand unified theories, such as SU(5). It also set out to obtain precise
measurements of solar, atmospheric and supernova neutrinos. The fiducial mass
of SK was increased over that of Kamiokande by a factor of ten (from 2140 tons
to 22,000 tons) and the number of photo multiplier tubes (PMT) increased from
948 to 11,200 (20 inch), doubling the overall light sensitivity. The SK experiment
[100] obtained the ratio of measured to predicted neutrinos of 0.358
+0.009 ( ) +0.014 ( )-0.008 stat -0.010 syst .
Using heavy water, the SNO [101], located in the Crieghton Mine (near
Sudbury, Canada), charged current and neutral current reactions measured all
types of neutrinos through the deuteron reactions ve +d ~ p + P +e- , and
vx +d ~ vx + P +n , as well as the neutral neutrino electron scattering reaction
V x +e- ~ V x + e- [102]. Not only could the electron, and combined mu and tau,
neutrinos be directly measured using the unique reactions on deuterium, but the
anti-electron neutrinos could also be measured through the reaction
Ve +d ~ n +n +e+. The SNO detector is, therefore, able to identify all types of
neutrinos through either free neutrons or relativistic electrons where the thermally
captured neutrons are identified after they emit gamma rays that subsequently
produce relativistic electrons through Compton scattering. Through these unique
reactions, SNO obtained direct evidence that electron neutrinos are being
95
converted into other flavors on their way from the solar interior to the surface of
the Earth.
The terrestrial neutrino experiment, KamLAND, using man-produced anti
neutrinos from the distribution of nuclear reactors in an approximate 180 kIn
radius around the Kamioka liquid scintillator detector near Tokyo, was able to
probe the neutrino oscillation parameter space with significantly higher precision
and show that neutrinos are massive and that neutrino flavor mixing does indeed
occur. The results from KamLAND [103], in conjunction with solar neutrino
data, singled out the large mixing angle (LMA) MSW solution.
6.2 Experimental Findings and Upcoming Studies
Numerically calculated spectra of neutrinos emitted from the Sun provide
a remarkable way to investigate the physics of the solar interior. (See Figures 16
& 17.) Solar neutrino data combined with standard solar models and
measurements from helioseismology [104] largely confirm our physical
understanding of the energy emitting nuclear reactions in addition to providing a
strong foundation to better describe many properties of the Sun and its structure,
energy transport and evolution with an unprecedented degree of precision. For
example, because of the amazing accuracy available through helioseismological
observations, even the tiny relativistic effects due to the partially degenerate
96
electrons in the core have been detected [63]. The antineutrino reactor results
from KamLAND have essentially eliminated all of the alternative explanations for
solving the solar neutrino anomaly leaving only the LMA MSW solutions.
Because of the dramatic advances in neutrino physics over the past five (5) years,
increasingly detailed and exacting inquiries can now be conducted to further
probe the inner working of the Sun. For instance, some researchers have argued
that because of the level of precision recently obtained in neutrino experiments,
solar density fluctuations may be probed with a sensitivity that even
helioseismology cannot reach [57,105].
In the three neutrino framework, the six oscillation parameters ~m12,
~m13, 812, 813, 823 , and bcp have been determined [106] as having the approximate
values ~m12:::: 7 X 10-5 eV2, ~m13:::: 2 X 10-3eV2, 812 :::: 33°,813 :::: 45°, 823 ~ 13°
(an upper bound when ~m13 :::: 2 X 10-3eV2) and bcp is, as of yet, unknown.
Future experimental findings from the KamLAND long-baseline experiment to
MINOS should provide increasingly accurate data in determining ~m:2 while new
low energy experiments, such as Borexino, and new nuclear detector experiments
should give us a significantly improved value for the solar mixing angle [107].
With an improved value for ~m:2' more precise measurements of solar physics,
neutrino matter effects, neutrino electromagnetic effects in addition to future tests
ofCPT invariance, and the neutrino sector MNS matrix [108] may become
reasonably well known in the not too distant future. Using KamLAND's findings,
the solar neutrino anomaly may also be investigated through sub-leading effects
97
such as sterile neutrino interactions [109], spin-flavor precession [110] and
neutrino decay [111]. Cosmological studies, such as that from the Wilkinson
Microwave Anisotropy Probe (WMAP) have found that for three degenerate
neutrino species, the limit of their masses is less than 0.23 eV thereby constraining
the total number of neutrinos to three with a combined mass of less than 1 eV
[112].
Perhaps the most difficult, as well as the most important, future neutrino
investigations will be to obtain accurate values of the various neutrino masses and
to design experiments to see if the CP violating phase in the MNS matrix is non
zero. Another key question along these lines is whether neutrinos are Dirac or
Majorana particles. In addition to the on-going experiments to find values for the
various neutrino masses, such as from tritium decay, neutrino-less double beta
decay and large-scale structure of the universe measurements, there have been
attempts to obtain neutrino masses from measurements of those emitted during
the processes associated with supernova explosions [64,113].
Unlike the case of the Sun, neutrino emission occurs in the core collapse
of massive stars in two steps. In the first step, electron neutrinos are emitted
during neutronization (when electrons and protons are compressed together under
extremely high pressure and undergo electron capture via p + e- ~ n + ve), and in
the second step, following the collapse proper, neutrinos and anti-neutrinos of all
types are emitted in thermal processes (e.g., e+e- -+ vii). The first step proceeds
adiabatically at higher density where flavor conversion occurs in the H-resonance
98
region where the relevant oscillation parameters 813 and ~m13 are obtained from
atmospheric neutrino studies. The second, nonadiabatic, low-density step occurs
in a lower density region, known as the L-resonance which is described by the
same mixing angles and mass splittings as for the Sun, i.e., 812 and ~m12 [114].
In particular, the electron neutrinos emitted during neutronization [91]
have average energies of about 13 MeV and the above description of SN neutrino
processes requires that the normal mass hierarchy is valid, i.e., the neutrino
masses are ordered such that m3 > m2 > mt. (See Figure 20.) It is found that
conversion probabilities for the first step are largely independent of energy and
that the adiabatic H-resonance takes place in the stellar region between R =0.03
Ro and 0.05 Ro. (It is assumed that the pre-supernova proto-neutron star has the
same radius as that of the Sun.) Using the above parameters for the H-resonance
conversion MSW effect, the electron survival probability can be determined using
a pre-supernova density profile similar to that given in Figure 21. Just as in the
case of the Sun, capture and analysis of emitted SN neutrinos can further our
understanding of neutrino physics and the explosion mechanism of core collapse
of massive stars. Unfortunately, the rate of core collapse supernovae in our
galaxy is approximately 2 ± 1 per century [64].
99
7.0 The Influence of Electron Degeneracy on the MSWEffect
Three (3) different methods were used to determine the influence of
degenerate electrons on the electron neutrino flavor conversion mechanism in the
solar interior: 1) Using an exponential approximations to the solar density
profiles, analytical solutions were computed to determine the average electron
neutrino survival probability of neutrinos exiting the solar surface; 2) by
numerically integrating the propagation equation using a) a common data block
density profile (SUN1) which gave the average neutrino survival probability at
the solar surface, and b) a stepwise calling routine (SUN2) which read in data
from two different standard solar models to calculate the electron neutrino
evolutionary profile as a function of solar radii.
While numerically integrating the neutrino propagation equation has the
advantage that its final results can be directly compared with experimentally
measured neutrino event rates, analytical solutions are more transparent --
revealing more of the underlying physical processes associated with neutrino
flavor conversion in matter.
100
7.1 Analytic Solutions of the MSW Effect in the Sun
By transforming the differential and integral equations describing the time
development of the electron neutrino flavor eigenstates into that of a confluent
hypergeometric differential equation, exact analytic solutions for the cases of
linear and exponential solar density profiles can be obtained. With a suitable
change in variable, an equation, known as the Whittaker equation, is arrived at
whose general solution can be represented as a linear combination of Whittaker
functions [115].
C. Zener arrived at the general equation describing the non-adiabatic
transition probability between two electronic states, for the case of polar and
homopolar states of certain molecules. He achieved this by combining the two
simultaneous first order differential equations of pure polar and pure homopolar
states into a single second order differential equation [116]. With an appropriate
transformation from real to complex variables and suitable substitutions, the
equation was put into a standard form, known as a confluent hypergeometric
differential equation, i.e., xy" + (c - x)y' - ay =0 with one regular singularity at 0
and one irregular singularity at 00. These solutions can be written as
y =bllF\(a;b;x) +b2U(a;c;x)
101
where 1F1 and U are confluent hypergeometric functions of the first and second
kind, respectively.
As a function of the polar and homopolar inter-nuclear distance (in the
case of molecules), the two eigenvalues initially approach and then move away
from one another with exchanged eigenfunctions. When the two states approach
each other with a velocity that violates the adiabatic theorem, there is a finite
probability that there will be an abrupt transition between the two states. The
linear combinations of polar and homopolar states can be expressed as
where H is a Hamiltonian operator, E, the energy eigenvalues for the polar, <1>1, and
the homopolar, <1>2, states. The probability of transition between the polar and
homopolar states was found by Zener to be P =e -210/ where
2" 2 1
r= hc12ld j'-(c -cdt 1 2
Notice that only the diagonal elements appear as functions of time. Therefore,
Zener's paper on the non-adiabatic level crossing problem dealt with transitions
between the ground state and the excited state of a two level system whose
instantaneous eigenvalues approach one another because of the external influence
of a time dependent term in the Hamiltonian.
102
That same year, L.D. Landau obtained a similar formula for the transition
probability [117] using an extension of the semiclassical WKB approximation!
which can be extended to describe complex, classical trajectories [118]. The
WKB, or semiclassical approximation method uses a sinusoidal approximation as
a real wave function solution to the Schrodinger equation where the space integral
of the classical momenta is the phase integral. The semiclassical approximation
has a wide range of application: Gamow, Condon and Gurney used this method in
their theory of alpha decay; in addition, it provided the staring point for
determining the classical solutions of the quantum chromodynamic field
equations in Euclidean space-time, known as instantons.
To apply the WKB approximation to a potential, one needs to find the
phase integral S as a function of the energy W. The WKB solution, attained
through the correspondence with the classical solution to the 1D Hamilton-Jacobi
equation for a stationary state, [119] is written as
_ x
S(x,t) =W(x) - Et =±fdx'~2m[E - Vex)] - Et
where W(x) is known as Hamilton's characteristic function and, Hamilton's
principle function, S(x,t), is separable for constant H. Accepting the above
1 Named after G. Wentzel [Zeits.J Phys. 38 (1926) 518], H.A. Kramers [Zeits.J Phys. 39 (1926)828], and L. Brillouin [Comptes Rendus 183 (1926) 24]. It is based on a method that is similar toa theory advanced by H. Jeffreys [Proc. London Math. Soc. (2) 23 (1923) 428]. Lord Rayleighdeveloped the mathematical connection made on either side of the turning points for thepropagation of an optical disturbance in a nonuniform medium [Proc. Roy. Soc. A86 (1912) 207].A general approach of the problem was first formulated by J. Liouville [Jour. de Math. 2 (1837)168,418] based on a function created by G.B.Airy in his description of rainbows [Trans. CambroPhil. Soc. 6 (1849) 379]. So, the method may also be called the WKBJRL method.
103
correspondence, the WKB approximation allows for the stationary state solution
to the Schrodinger wave equation to be given by2
{canst } [(i)Xf ,~ iEt]If/(x,t)= [E_V(X)]1/4 exp ± Ii dx v2m lE-V(x')J-p;
The difficulty arises in trying to match the two solutions across the classical
turning point in the forbidden region. The WKB procedure entails linearly
approximating the potential across the turning point, solving the differential
equation in terms of Bessel functions and, then, matching solutions on either side
of the classical turning point by choosing suitable integration constants.
Landau, in finding an approximate solution for an atomic quantum
mechanical level crossing problem, transformed the equation by reducing it into a
simpler form by using an approximate solution to the wave equation instead of
beginning with the exact solution and then attempting to approximate it. Since
the wave equation is assumed diagonal in the adiabatic approximation, the
solution of the equation
where IfFm =(:;Jand 1'1m =(A - 1'1 cos 28)' + (1'1 sin 28)' , can be found from the
exponential of the integral of the diagonal elements [120], i.e.,
2 The analogy is made according to the prescription If/(X,t) =~p(x,t)eiS(X,t)/h .
104
A=&±iZ8
InPlZS =- ~Irn J ~(A-Llcos28Y + (Llsin 28)2d.x.A=6cos2B
Thus, from the above integral, the level crossing probability for the electron
density distribution can be obtained for the case of an exponential solar density
profile by introducing A oc exp(-r), leading to In«(':) ~1- tan' () .-y -
2
In other words, the form that LZS3 hopping probability takes can be written as
[121]
where, for exponential density profiles, the correction function Fn(8) is equal to
1-tanZ8. Landau's method gives only he leading term, or the exponential part, of
PLZS for arbitrary density distributions.
In solving the above integral, the contour is deformed to make the
integration simpler by beginning with the real axis near the point A =Llcos28,
along one side of the branch cut and around the branch point A =Lle±iZ8 =Llcos28
± i sin28 and, then, down the other side [120]. So, beginning with the point of
complex time where the eigenvalues are equal, the variation in the path of the
state is followed over into the complex plane from where it begins on the real axis
to where it ends (also on the real axis) revealing the quantum nature of the
3 E.C.G. StUckelberg also introduced the method that same year for the problem of interbandtunneling in semiconductors, Helv. Phys. Acta 5 (1932) 369.
105
transition, i.e., taking place in complex time [122]. Thus, the LZS level crossing
probability determines the probability, for example, of the state Iv2) to cross over
to the state IVI) in a manner which is analogous to that of quantum mechanical
tunneling through a barrier.4
A number of authors have obtained a variety of approximate solutions in
the case of linear [51,123] and exponentially [124] varying solar density profiles
to arrive at the average electron neutrino survival probability exiting the solar
surface. Originally, the electron neutrino survival probability was first given by
S. J. Parke in terms of the Landau-Zener-Sttickelberg "hopping" probability, PLZS,
for transitions between matter mass eigenstates for single (and double) resonance
crossing using a linear approximation of the solar density profile [51]. Using the
Landau-Zener approximation for a linear density profile, Haxton [125] found
formulae for the probability of detecting an electron neutrino far from the Sun.
Additionally, for the case of a linearly varying solar density for two neutrino
oscillations, S.T. Petcov solved the neutrino evolution equation exactly in terms
of Weber-Hermite functions [126].
Later, Petcov provided an exact analytic expression for the two flavor
probability amplitude in matter using an exponentially varying electron number
density in terms of linear combinations of confluent hypergeometric functions,
WK,~ and MK,~, to solve the Whittaker differential equation:
4 The LZS theory can be used in applications related to molecular dissociation, molecular andatomic collisions and during electron transfer in biologically important molecules.
106
1 [ 1 2])d 2 1 k "4 -,u-2+ --+-+ 2 Ae(t,tO) =O.dz 4 z z
In the above differential equation, Ae (t,to) is the probability amplitude for an
electron neutrino. Petcov's solutions to this equation were given in terms of
asymptotic expansions of Whittaker functions for large values of Izl.5
S. Toshev [127], using a similar analysis, expressed the Whittaker functions in
terms of confluent hypergeometric functions for the case when Izi is very small.
A summary table of the electron neutrino survival probabilities using
analytic solutions for the exponential solar density profile approximation along
with numerical results using a common data table (SUN1) and stepwise solutions
(SUN2) to the neutrino propagation equation is given below.
Table 8. Analytic and Numerical Results ofP(ve~ve) 6
Source P(ve~ve) 812 =30° P(ve~ve) 812 =33°Parke and Walker 0.25000000 0.29663167Pizzochero 0.25000177 0.29663663Petcov 0.25022300 0.29663167Krastev and Petcov 0.25001812 0.29664549SUN1 (block data) 0.3619868 0.2900484SUN2 (stepwise) -0.375 [pmax_pmin (ve~ve)] -0.330T [pmax_pmm]
t The lower half of the survival probability envelope drops by about 0.09, so 0.375(ave)-0.0912
(ave) - 0.330.
5 See E.T. Whittaker and G.N. Watson, §16.3: "The asymptotic expansion ofWK,ll when Izi islarge" in [ref. 115, p. 342].6 NOTE: ~m2 = 7.1 x 10-5eV2and <Ev(8B» = 10 MeV.
107
The analytic solution for the case of Parke and Walker [124] was obtained using
the formula
p(Ve ~vJ=1/2+(1I2-PJcosOM cosO
where
The values obtained from analytic expressions gave an average electron neutrino
survival probability P(ve-7Ve) = 0.25 for e= 30° which is reasonable since
P(Ve-7Ve);:::: sin 2efor the adiabatic case and P(ve-7Ve) ::::; 0.30 for e= 33° which
is about the same as the most recent SNO result where P(ve-7Ve) = 0.306 ± 0.026
(stat) ± 0.024(syst) [102]. Notice that the numerical value given by SUN1 for the
LMA MSW solution (8m2 = 7.1 x 10-5 eV2, e= 33°) is within 2% that obtained
from the analytic solutions using the exponential solar density approximation.
(See Figure 34.)
7.2 Numerical Calculations of ve Evolutionary Profiles
A straightforward calculation of the electron number density profile as a
function of radius with and without electron degeneracy was performed for a
given number of discrete radii required for the particular standard solar model
chosen. By using the appropriate electron number density profiles in the
numerical subroutine SUN2 (a modified version of David Casper's subroutine,
108
MATTER -- which calculates the probability of re-conversion of v~ -7 Ve of J!-
neutrinos passing through the Earth), evolutionary profiles of the electron survival
probability for electron neutrino propagation through the Sun were obtained. By
comparing the results for the cases with and without electron degeneracy, the
influence of electron degeneracy on the MSW effect in the Sun was identified as a
function of solar radius.
The two programs, SUN1 and SUN2, numerically integrated the neutrino
evolution equation to determine the electron neutrino survival probabilities using
the three neutrino algorithm for a uniform medium given in [129] using
"[Il 2ER .. -MfO.. } . 2probability amplitude where Xij =LJ IJ 2 IJ -IMk,L/2E.
k' k*k' /).M kk'
The three-generation mixing matrix relating the mass and the flavor
eigenstates in the original program MATTER, although unitary, did not have the
proper values for the given elements in the matrix, expected to be of the form
costAsin 02
.J2sin 03
.J2
-sinO\cos 02
.J2cos 03
.J2
o1
-.J21
.J2
Therefore, the mixing matrix in D.W. Casper's Ph. D. Dissertation [62] was
introduced into the routine MATIER in place of the one provided in his
numerical program.
109
Neglecting any CP violating phases, a three generation mixing matrix can
be obtained by matrix multiplication between the three separate rotation matrices,
R12(e-/l), R13(e-T), and R23(/l-T) where U = R23 R13 R12 and
lcosO, sinO! nR!2 = -s~O! cosO!
0
lcosO,0
sinO,JR13 = 0 1 o ,
-sin 02 0 cos O2
R~ =l~0
Si:O,Jcos 03
- sin 03 cos 03
so, using c = cos 8 and s = sin 8,
U =l~0
°r2 0 S1 c1 sl OJ
c3 s3 0 1 o - sl c1 0
-s3 c3 -s2 0 c2 0 0 1
u~l~0 °Ic2c1
c2s1
S:Jc3 s3 -sl c1
-s3 c3 - s2c1 - s2s1 c2
lc2c1
U = - slc3 - s3s2c1
8381- c3c2c1
c2s1
c3c1- s3s2s1
- s3c1- c3s2s1
s2 Js3c2
c3c2
which was the matrix that was used in the modified routines EARTH, SUNI and
SUN2.
110
The electron survival probability obtained using the routine EARTH was
now found to be 0.975 which is in good agreement with values expected for the
re-conversion of mu-neutrinos into electron-neutrinos, i.e., P(v~-7Ve) = 2.5%.
After the above mixing matrix was introduced into the common block routine
SUN1, an electron neutrino survival probability of electron neutrinos propagating
through the Sun was found to be P(ve-7Ve) = 0.362 for 8 = 30°. In addition,
noticeably improved resonance curves were obtained in the output from the
program SUN2. (Compare Figures 36 and 37.)
The evolutionary probability profiles (for the SSM JCD1987) and
subsequent percent differences in P(ve-7Ve) as a function of solar radius are
shown in Figures 38 - 43. Following the lower edges of the probability
trajectories, matter enhanced resonances can be clearly seen in the region between
0.1 Ro and 0.3 Ro with a mean value around R = 0.2 Ro. When examined in
more detail, the vacuum oscillation lengths (in the region near R = Ro) are found
to be about 350 km. Using the Standard Solar Model BP2000, Figures 49 - 54
show the probability evolution and percent differences in P(ve-7Ve) with an
increased step size (discemable because of the lack of a darkened region around R
= Ro) and change in mixing angle (from 8 = 30° to 8 =33°). The lower edge of
the probability envelope dropped significantly from about 0.26 to roughly 0.17 - a
difference of approximately 0.09. (Since the survival probability is obviously
falling, the average of this value is therefore subtracted from that for the early
estimate.)
111
Nevertheless, as with the earlier percent differences in P(Ve7Ve) (Figures 40
and 43), any influence due to the electron degeneracy on the MSW effect (Figures
51 and 54) are entirely washed out by R =0.6 Ro, so there is no observable
difference in P(Ve7Ve) by the time the electron neutrinos reach the solar surface.
(The more gradual falling away of the probability difference in the region 0.5 Ro
in Figures 51 and 54 is a consequence of improved values for the FD integrals in
that region.)
A comparison was made using the output from SUN2 with some plots in
the available literature (See Figure 22 (Smimov's Figure 9).) Some of the
evolutionary trends as a function of solar density can be seen: 1) for Figures 44
and 45, there is a noticeable broadening toward the solar surface (at n =0),2) for
all of the figures (Figures 44 - 47), there is a widening of the probability envelope
with decreasing neutrino energy, and 3) there is also a steady loss of curvature as
Ev is lowered in both the SUN2 plots and Smimov's figures. (It is difficult to
compare the two lower energy graphs, however, because Smimov's density
regions have now shifted to positive values.)
Numerical calculations of the evolution of P(Ve7Ve) obtained from the
above programs have a number of features consistent with those in the literature:
(1) the matter enhanced resonance can be clearly seen in the region R =0.2 Ro,
(2) the difference between the minimum and the maximum electron neutrino
survival probabilities are within the range of other experimentally published
results (e.g., P(Ve7Ve) =0.306) [102], (3) the probability for re-conversion of v/-l's
112
passing through the Earth is the range of predicted values [130,131], (4) the
vacuum oscillation lengths found numerically (Lo - 350 kIn) are comparable with
those calculated (Lo - 300 kIn) and are correct to order of magnitude for those
measured at KamLAND (L - 200 kIn), and (5) the electron neutrino evolutionary
plots as a function of energy exhibit features that are similar to those given in
[54].
However, the numerical results from SUN2 have maxima and minima
after the resonance region that is consistently too large. This unwanted effect may
be an artifact of forcing the routine to read in SSM data stepwise, instead of
through a common block, because the routine SUNI gives good estimates of the
electron neutrino survival probability for electron neutrinos traveling through the
Sun, in addition to acceptable P(vlt ~ ve) re-conversion values for the case of
neutrinos passing through the Earth.
The modifications that were made in the numerical routine to determine
the electron survival probabilities in the case of SUN2 required introducing some
procedures that read in the data from a given SSM and allowed for two cases with
and without electron degeneracy to be calculated. The degeneracy pressure was
extracted from the SSMs with the help of the ratio of the Fermi functions
2/ 3(F3I2) giving the percent ratio of the pressure with and without electron
F1I2
degeneracy [ref. 17, p. 97]. Because the electron number density is directly
proportional to the pressure (from the ideal gas law, Pe=nekT), the same ratio of
113
Fermi functions provided a convenient way to obtain the electron neutrino
survival probabilities for the cases with and without degeneracy for a given solar
radius by directly subtracting out the electron degeneracy component from the
two different solar models (BP2000 and JCDI987).
In conclusion, I) the exponential equation describing the density profile
for the Parke and Walker analytic formula was modified to include degenerate
and non-degenerate cases. The only changes in the resulting average electron
neutrino survival probability were in the tenth decimal place, i.e., no differences
were seen in either of the final electron neutrino survival probabilities; 2) no
changes in P(ve~ve) were observed when common block density profiles with
and without electron degeneracy were introduced into the numerical routine
SUNI; and 3) calculations of the electron neutrino survival probability as a
function of distance/time found no changes with and without electron degeneracy
in P(ve~ve), once the electron neutrinos reached the solar surface. Numerical
values given by SUNI using the LMA MSW solution, i.e., P(ve~ve) =0.290, are
within 2% of that obtained using analytical methods, i.e., P(ve~ve) =0.297. Both
of these values are within 6% and 3%, respectively, with the most recently
reported experimental results from SNO: P(ve~ve) = 0.306 ± 0.026 ± 0.024.
114
8.0 Conclusion and Future Prospects
The continual progress in experimental solar neutrino physics, beginning
with the pioneering radiochemical argon experiments, have recognized the Sun as
a superb astrophysical system for advancing low energy particle physics, nuclear
physics, neutrino astronomy and, even, cosmology. Although Davis and company
were initially interested in verifying the nuclear reaction hypothesis, -- which
attempts to describe the Sun's power generation in terms of a particular sequence
of thermonuclear fusion reactions (i.e., the pp chain or the eND cycle)-- the
deficit of measured electron neutrinos observed in the Homestake argon detector
inaugurated the present period of v research marked by phenomenal growth in a
number of fields related to the physics of the stars and neutrinos.
In what turned out to be a colossal effort, investigators diligently sought to
improve upon the solar models which some believed had already reached a
developmental plateau by the 1960s. Other researchers pursued increasingly
sophisticated experiments to reduce the uncertainties of the details associated with
nuclear cross sections. In parallel with these developments, ever more refined and
reliable solar neutrino detectors experiments were built, such as the water
Cerenkov detectors, Kamiokande I and II; the radiochemical gallium detectors,
GALLEX and SAGE~ the giant SuperKamiokande light water detector~ and the
heavy water detector SNO which measures elastic scattering, neutral current and
charged current reactions - ultimately, allowing it to obtain direct evidence of
115
solar neutrino flavor conversion. There is also the neutrino accelerator
experiment, LSND (Liquid Scintillating Neutrino Detector), and the follow-up,
BooNE (Booster Neutrino Experiment) which study mu to electron oscillations
and anti-neutrino oscillations with the possibility of confirming the existence of a
fourth neutrino. Finally, the precision results from KamLAND's terrestrial
antineutrino reactor experiment in conjunction with solar neutrino data have
essentially eliminated all of the contending explanations for the solar neutrino
problem except the LMA MSW solution with a 99.73% confidence level [132].
These and other scientific advances were inspired by the solar neutrino
problem and the discovery by Mikheyev and Smimov of the phenomenon of
density dependent resonant neutrino flavor conversion. By the end of the 1980s,
many researchers realized the importance of the MSW effect as an elegant way to
resolve the solar neutrino anomaly. Because of these steady experimental and
theoretical advances, ever more detailed and demanding studies and experiments
are presently being pursued (e.g., Borexino). Some investigators have argued
that, because of the increasing precision arising from the advanced degree of
integration between astrophysics, nuclear and particle physics and solar neutrino
and solar modeling studies, a more exacting assessment of the solar (and pre-SN)
interior may be possible through neutrino astronomy -- beyond that even available
through helioseismology [57, 105].
116
The phenomenology of neutrino mixing and nonzero neutrino masses,
especially the identification of the LMA MSW solution to the solar neutrino
problem (and the results from WMAP), have had a significant impact on the
development of some grand unified theories. In retrospect, it appears that purely
leptonic interactions offer good physical systems for investigating astrophysical
applications of quantum field theories [149] because they avoid many of the
difficulties associated with quark-related interactions and they exhibit sufficient
intricacy to make them interesting, research-worthy phenomena.
8.1 Neutrinos and Cosmology
While the solar neutrino problem has been convincingly solved, the
determination of the absolute masses of the neutrinos has proved elusive. We
now know, however, that neutrinos do indeed have mass because of atmospheric
neutrino vJ1 f-7 V T oscillation measurements made at SK (hep-ex/9807003) and
direct measurements of converted solar neutrinos to other generations performed
at SNO (nucl-ex/0106015). Advanced experiments are presently being conducted
to obtain significantly improved values for the oscillation parameters, as well as
experiments to probe the absolute neutrino mass scale, such as the dedicated
tritium decay measurements (mv< 2.2 eV, Mainz) which are gradually pushing
down the upper mass limits (as the proposed KATRIN experiment with an
expected mass sensitivity of around 0.3 eV), in addition to future searches for
117
neutrinoless double beta decay (which require massive Majorana neutrinos) with
anticipated mass sensitivities of 0.01 eV [133] and mee < 0.35 eV [134].
Still, no lower bounds to neutrino masses have yet been experimentally
verified, nor has the determination been made whether or not neutrinos are
Majorana, Dirac or Weyl particles. In addition, the total number of families of
neutrinos still remains an open question. Core collapse of massive stars, such as
SN 1987A (which found my < 20 eV), may provide the best means for obtaining
mass limits from nearby (- lOkpc) future galactic supernovae [135]. Recent
precision cosmology studies have helped close in on the upper bounds of these
absolute neutrino masses (e.g., Lmy< 0.7 eV, WMAP), so that cosmology will
most likely play an important role in interpreting neutrino masses. Perhaps, even
gamma-ray bursters (GBR) may prove to be another viable astrophysical source
for studying the physics of neutrinos [136] through the detailed information that
they can provide concerning the structure and composition of pre-SN stars [137].
Conversely, the neutrino mass scale arrived at through the see-saw model
[138] (my - 0.008 eV) has provided theoretical justification for recent models of
large-scale structure of the universe. Some cosmologists, who consider a scalar
field description of the cosmological constant, A, have argued that the neutrino
mass scale for the MSW solution offers an explanation for why the vacuum
118
energy is dynamically important in the present epoch. 1 In such dynamical A
models (where pseudo-Nambu-Goldstone bosons are protected by the fermion
chiral symmetry), using m =0.005 eY, f =1.885 X 1018 GeY (the instantaneous
expansion rate), and <I>/f = 1.6 (the ratio of the scalar field to the expansion rate),
the scalar field density parameter was found to be Q<I> =0.6 [139]. (Compare this
value of the scalar field density parameter with Q A =0.67 obtained by the High-z
Supernova Search Team [158] and WMAP's value of QA =0.73 ± 0.04 [140].) 2
Table 9: Neutrino Properties
Degenerate neutrino mass < 0.23 eY tElectron neutrino mass < 2.2 eY (Mainz)Muon neutrino mass < 170 keY (PRD 66(2002) 010001)Tau neutrino mass < 15.5 MeY (Aleph & CLEO)Neutrino half-life 1.57 x lOL
:l yrs (IGEX)Magnetic moment for Ve < 1.8 X 10-10 IlBMagnetic moment for v Il < 7.4 X 10-10 IlB (LAMPF)Magnetic moment for V1: < 4.2 X 10-7 IlBtan2
8 12 0.41 (Bahcall, JHEP 11 (2003) 004)
/}.m~ol 7.3~~::x 10-5 ey2 (ibid.). 28 > 0.92 [3]sm 23
/}.m~tm 2.0 x lO-J eYl. [3]
tan28 13 < 0.16 [3]
OCP - 0 (assumed)
t D.N. Spergel et aI., "First Year Wilkinson Microwave Anisotropy Probe (WMAP)Observations: Determination of Cosmological Parameters," ApJS, 148 (2003) 175.
1 Other researchers, inspired by the similarity between the neutrino mass scale and that of the darkenergy, have treated the neutrinos as mass varying so that they behave as a negative pressure fluid[154].
2 The most recent findings from the European Space Agency's XMM-Newton orbiting x-rayobservatory indicate that, according to their analyses, the percent of dark energy in the Universe isless than 15% [128].
119
An alternative approach to the grand unified theoretic treatment of the see-
saw mechanism for explaining the origin of the extremely small neutrino masses
arises in left-right symmetric models (e.g., SU(2k x SU(2)R xU(l)) where the
neutrinos are found to have arbitrary but finite masses [141]. In these models
spontaneous parity nonconservation provides an explanation for understanding the
very small neutrino masses due to the fact that the suppression of V + A currents
2
are proportional to the neutrino masses. In particular, by using mv = gme andh3mWR
mWR - 300 GeV, the upper bounds on the masses of the three families of
neutrinos are found to be mv ::; 1.5 eV, mv ::; 56 keV I mv ::; 18 MeV -- valuese I" T
which compare favorably with recent experimental results: mVe
::; 2.2 eV (Mainz),
mv ::;170 keV,and mv ::;18 MeV (Aleph).I" T
Alternatively, if the lightest left-handed neutrino mass has a value below
mVe
::; O.leV, then cosmological baryon asymmetry can be achieved as long as
lepton number generation takes place in a preceding epoch where, in such non-
GUT models, the observation of a neutrino mass above mVe
- O.leV in a OvJ3J3
decay experiment would lead to the conclusion that the GUT baryon number
generating scenario must not be viable [142].
120
In minimal supersymmetric standard models supplemented with two U(l)
symmetries, it is shown that one of the symmetries breaks at 1015 GeV while the
other is broken in accordance with the MSW solution to the solar neutrino
problem through a see-saw mechanism [143]. Some researchers find that a
relatively small asymmetry between the electron neutrinos and the antielectron
neutrinos can significantly impact the ratio of the neutron to proton ratio in the
early Universe in the presence of additional degrees of freedom (i.e., including a
new energy density) [144]. By introducing three right-handed neutrinos, other
studies have found approximate values for absolute neutrino masses [145].
Altarelli and Feruglio believe that the smallness of the neutrino mass is probably
related to the fact that the neutrinos are completely neutral and are Majorana
particles [146].
In cosmological models that describe baryogenesis through leptogenesis,
the departure from equilibrium in the early Universe (the third Sakharov condition
where Band CP violation are the other two) occurs through the decay of heavy
neutrinos, i.e., through the Yukawa interaction of heavy Majorana where
yC ~ fH and yC ~ fH (with CP violation). The nonconservation of L is a
consequence of the ilL =2 term that creates the Majorana mass. The mechanism
of baryogenesis through leptogenesis is disfavored if Imvl ~ 0.1 eV, whereas the
degenerate neutrino model with Imvl ::; 0.23 eV is favored following the results
121
from KamLAND and WMAP [ref. 146, p. 9] where an experimental limit of the
Majorana mass has been given to be around 0.2 eV [147].
In nonlocal theories of baryogenesis, the bubble wall -- an expanding
region of the early Universe where the high temperature phase changes into a low
temperature phase -- interacts with the fermions with unbroken phase through a
chiral to baryon asymmetry carried by quarks and leptons. In particular, because
of the large Yukawa coupling, the main contribution to the conversion of the
chiral asymmetry to the baryon asymmetry comes from the top quark and the tau
lepton [ref. 143, p. 1486].
Even though neutrinos do not appear to have the requisite mass to account
for the closure of the Universe (-20 eV), they are of cosmological significance
because of tantalizing clues that they may hold the key to 1) the matter-antimatter
asymmetry of the Universe, 2) cosmic dark energy and 3) universal dark matter
(through their ostensible supersymmetric partner- the neutralino).
Thus, in leptoquark models, the smallness of the neutrino masses are a
consequence of processes that violate lepton number conservation so the observed
values of baryon asymmetry appear to be intrinsically bound up with neutrino
phenomenology [ref. 146, p. 10].3
3 For more details concerning the fundamental theory of neutrino masses and mixings, see [151].
122
8.2 Neutrinos and Stellar Physics
The recent advances in neutrino astronomy, especially those pertaining to
the Sun and SN 1987A, have given us an improved understanding and, in
combination with other experiments and studies, added confidence for
approaching more complex astrophysical systems. The theory of partial
degeneracy offers an effective tool for probing astrophysical objects because it is
based on well-understood physics and so introduces little error into calculations
dealing with the Sun, SNe and stars of various masses during their diverse
evolutionary phases. The physical insights that the MSW effect has provided (in
accurately describing relevant solar processes) offers increased assurance for
pursuing neutrino studies of more challenging astrophysical objects and events
such as those pertaining to pre-SN stars and the mechanism of core collapse of
massive stars. In addition, data from future neutrino experiments may possibly be
used to quantitatively investigate the existence of solar density fluctuations. In
this regard, investigations of density dependent neutrino flavor conversion may
allow for unparalleled profiling of the solar interior.
Similarities in the underlying physics describing the Sun and massive core
collapsing stars offer unique opportunities for better comprehension of pre-SN
structure and core collapse processes as well as a means of obtaining more
accurate values for the absolute mass, decay rates, and magnetic moments of
neutrinos. The Sun, for example, which only has one physically allowable critical
123
density region for a given energy neutrino, can be thought of as a simpler version
of a pre-SN star whose H-resonance region can be studied by replacing the solar
density profile with the most accurately available pre-SN density profiles, the
solar neutrino oscillation parameters with those obtained from atmospheric
studies (i.e., ~m13 and 813), in addition to making any needed modifications in the
matter enhanced weak interacting potential [43].
Since the sustained effort over the decades, beginning with
Schwarzschild's solar modeling hand calculations in the 1940s to the incredibly
sophisticated contemporary solar model calculations (in addition to neutrino and
helioseismological findings), exceptionally detailed investigations of refined
astrophysical properties and phenomena are becoming increasingly common.
Consequently, because of the ability of neutrino astronomy to help quantifiably
characterize various solar properties, one should expect an ever more detailed
understanding of the physical processes underlying stellar evolution and structure
in the near future. On the other hand, astrophysical objects, such as supernovae,
and events, such as ORBs, emerge as stellar phenomena that are ideally suited for
advancing the study of low-energy, weak interaction particle physics through
upcoming experimental neutrino astrophysical studies.
124
Table 10: Solar Parameters (from Bahcall, Rev Mod. Phys. 54 (1982) 767)
Luminosity 3.86 x 1O.j.j (3.846 x 1O.j.j t erg sec-1
Mass 1.99 x 1O.j.j (1.989 x lO.j.j)a g
Radius 6.96 x lOw (6.95508 x lOW)t cmAge ~ 4.55 x 109 (4.57 X 109)a yrCentral Density 156 g (150)a cm-1
Central Temperature 15.7 x lOb KCentral Hydrogen abundance by mass 0.355Effective surface temperature 5.78 x lOj (5.77 x lO.j)a KPrimordial mass helium abundance 0.25 ± 0.01Primordial ratio of heavy elements to H 0.0228Neutrino flux from pp reaction 6.1xlO lU (5.95xlO lU )t cm-.t sec-1
Neutrino flux from llB decay 5.6xlOb(5.05xlOb)t cm-.t sec- 1
Fraction of energy from pp chain 0.985Fraction of energy from CND cycle 0.015
:j: from Allen's Astrophysical Quantities. 4th ed., Editor, A Cox. New York: AlP Press, 2000.t from J.N. Bahcall and C. Pefia-Garay, "A road map to solar neutrino fluxes, neutrino oscillation
parameters, and tests for new physics," JHEP 11(2003)004.a NASAIMarshall Space Flight Center/Solar Physics: http://science.nasa.gov/ssl/pad/solar/
Through neutrino astrophysics, 1) the pp chain has been identified as the
primary reaction sequence powering the Sun -a low-mass star(SAGE, GALLEX);
thus, verifying the standard solar model, 2) the fundamental physical processes
underlying supernova explosions has been verified following SN 1987A (1MB,
Kamiokande I, Baksan), 3) the LMA MSW solution to the solar neutrino problem
has been confirmed (KamLAND), and 4) the deep solar (and pre-SN) interior may
been quantitatively investigated in the near future to obtain a more detailed
understanding of the core nuclear reaction rates, temperature and composition.
125
8.3 Neutrinos and Degenerate Electrons
The effects of electron degeneracy on the MSW effect in the Sun opens a
window for describing the physics of neutrino propagation in other astrophysical
systems, such as stars in the red giant stage, white dwarfs, and pre-white dwarfs
because the underlying physics describing electron degeneracy is well understood
and highly relevant for investigating such evolved stellar systems. Additionally,
there are a sufficient number of exploitable similarities between the much better
understood processes associated with the Sun -- a low mass star -- and the vastly
more complicated physics describing more massive stars, as well as those in later
stages of their evolutionary cycle, such as those undergoing core collapse -- where
the electrons, the neutrinos and the neutrons may all be in degenerate states. One
parallel in the calculations of such obviously dissimilar objects (as low mass stars
and supernovae) comes about through the fact that the critical physical parameter
in elucidating the effect of the electrons on the exiting neutrinos is the electron
density profile of the stellar system under consideration. Because the varying
(stellar and planetary) density profiles are of decisive importance in causing
neutrino flavor conversion, analyzing the effects of neutrino conversion through
static "snapshots" of the density versus stellar radii of massive stars undergoing
core collapse as a function of time may offer a tractable way of approaching the
supernova problem.4 For example, any significant increase in neutrino luminosity
4 NOTE: Complications arise in attempting to describe neutrino propagation during supernova corecollapse when all the degrees of spin are included in the calculations. See [148] for more details.
126
in regions where the MSW effect and the RSF conversion mechanism take place
may be indicative of a means whereby converted neutrinos could revive a stalled
SN shock wave.
Questions regarding the effects of partial electron degeneracy on the MSW
effect in the Sun, red giants, Si-burning pre-SN and core collapsing SN offer a
simple but discerning way to gain a more detailed understanding of the inner
workings of stars covering a spectrum of masses at various stages during their life
cycle. Similarities in the physical processes of partial degeneracy in low-mass
stars, such as the Sun, and pre-SN core collapsing stars may provide opportunities
for an increasingly refined analysis of the solar interior and improved models of
pre-SN structure.
Following the identification of the LMA MSW solution as the most
probable mechanism for explaining the deficit of solar neutrinos and the
verification of the fundamental physics underlying the Sun and supernovae,
improved calculations of the electron neutrino survival probabilities and FD
integrals may be of interest for investigating density fluctuations in SNe [105] and
the solar core [57], as well as a means for quantifying the very small relativistic
effects which arise through the Sun's partial electron degeneracy [63].
Through the use of statistical quantum field theory [149], some
investigators have considered neutrino Cerenkov emission heating of degenerate
electron plasmas as a possible mechanism to revive stalled supernova shock
127
waves [24]. Since collisional damping is reduced in the case of a degenerate
electrons gas, neutrino induced electromagnetic wave heating becomes a viable
means of solving the supernova problem because the degenerate electrons reduce
the Debye screening length -- leading to a suppression of Landau damping. For
such neutrino induced heating of the plasma to take place, the magnetic field
outside the neutrinosphere must be of the order of B ~ 1015 G and the thermal
instabilities in the region must be significant. Electron neutrinos may excite
electrostatic waves through kinetic instabilities which may be important to
reviving the stalled SN shock wave because the neutrino-electron cross section
increases with the square of the neutrino energy [155]. Astronomical
observations of magnetic fields on the order of 1016 G [4] in conjunction with
turbulent instabilities, known to follow shock wave propagation [150], give this
regeneration scenario some plausibility,S
However, recent numerical hydrodynamical calculations of spherically
symmetric core collapsing supernovae indicate that non-electron neutrino
luminosities and energies increase when cooler degenerate electron gas is
replaced by the earlier, shock-heated nondegenerate electrons [156].
5 Other approaches have identified the Zimanyi and Moszkowski equation of state [152] in themean-field approximation as favorable to the delayed explosion mechanism because of theexistence of large trapped lepton concentrations [153]
128
In conjunction with the available solar neutrino data, the small influence
of the partial degeneracy in the Sun has been investigated. Analytic and
numerical solutions showed no observable variations in the electron neutrino
survival probabilities whether degenerate electrons were included or not in the
solar density profiles of SSMs. The fact that the partially degenerate electrons
were found to have no discemable effect on the inhomogeneous density
dependent flavor conversion of neutrinos exiting the solar surface was contrary to
expectations. These negative results could be due to 1) the crudeness of the
analytic and numerical models used, 2) the fact that, in the numerical routines, the
final results are a consequence of using the adiabatic approximation (in contrast
with their actual quasi-adiabaticity), or 3) perhaps the results reflect the nature of
the phenomenon, i.e., the small percentage of degenerate electrons in the region of
the solar core has, indeed, no influence on the MSW effect in the Sun.6
6 Table 2 in [72] implies that the non-ideal gas effects due to electron degeneracy in the OPALequation of state also have no noticeable influence, according to their studies.
129
APPENDIX A
Fierz transformation of the interaction Hamiltonian
Let 'If represent a four-component Dirac spinor, and r represent the set of
any physically allowable combination of the Dirac matrices {I, yll, yl!o.{, 'I, and
a llV} which stand for the scalar, polar vector, axial (or, pseudo) vector,
pseudoscalar and tensorial gamma matices, respectively. In four-component
notation, a four-particle interaction can be written as
or, more generally
where r K and r L correspond to any of the 16 combination of Dirac matrices.
After compacting the orthonormal trace formulae Tr{l} =4, Tr{yS ys}=4,
matrix M into a complete orthonormal set, i.e., M =L ~K r K ' the trace of theK
product of the matrix and the generalized gamma matrices is given by
Tr(MrJ =L~KTr(rKrJ.K
But, since Tr{rKrJ= 4JKL , then after collapsing the summation
130
In component form, the above coefficients can be written as
Rewriting the four particle interaction in terms of the components of the
respective column vectors and matrices,
and expressing the bilinear If/fJ (2)lf/o (3) as the matrix M fJo ' and repeating the
same normalization procedure using the trace formulae in the general case, we
find If/fJlf/0 =Lr;K (rK) ,so that
K fJO
j: 1 ( (K)) 1 K 1 K .~ K =- Tr M fJo r ofJ =- M fJo (r )0fJ =-If/fJlf/0 (r )ofJ Rearrangmg terms such
4 4 4 '
spinors anticommute, {If/fJ' If/o} = 0 , i.e., If/fJlf/0 = -If/olf/fJ ' allows the four particle
interaction term to be written as
Similarly, to move If/(4) to the left of If/ (3) introduces another minus sign, giving
Dropping the indices leaves
131
Thus the general Fierz transformation can be written as
(¥/(l)r K ¥/(2)X¥/(3)rdl/(4») = L;~~ (¥/(l)rM ¥/(4)X¥/(3)rN ¥/(2»)M,N
j:KL 1 (M K N L) 1 (J:' J:')where [30] ~MN =-Tr r r r r =- 4UMK 4uNL =1, so16 16
More specifically, for the case of electron-neutrino scattering
132
ApPENDIX B
Derivation of the Energy Rate Formula1
The reaction rate formula can be written as Rrx =If cr(v)vdnr(v)dnx(v)
where dnrCv) and dnx(v) represent the number of nuclei and particles per cubic
centimeter represented as volume elements in velocity space, cr(v) is the cross-
section for the reaction which describes the probability of the interaction as a
function of the particles' velocities. A Maxwell-Boltzmann (MB) distribution is
assumed valid because of the relatively low densities in the solar interior. (Yet,
see quotation on page 50 above.) Writing the particle number volume elements
in velocity space as an MB distribution, we find:
for the particle r and a similar expression for the target nuclei X. The reaction
rate formula becomes upon substitution
( )3/2 ( )3/2 ~ ~ [( 2 2 )}R =n ~ n -.!!!L ffexp - mrVr +mxvx (v)vd 3v d 3v
rX r 27lkT x 27lkT 2kT r xo 0
Using center-of-mass velocity V = (mrvr+mx vx)/(mr+mx) and the
relative velocity v =Vr - vx, we can substitute Vr =V + mxv /(mr + mx) and
1 See Huang and Yu, Stellar Astrophysics (1998)
133
Vx =Y - mxv /(mr + mx) into the equation for the conservation of kinetic energy
to obtain mrv2+ mxv2= (mr + mx)y2+ mv2where m is the reduced mass given
by m =mrmx/(mr+mx). In addition to these substitutions, the replacement of the
volume elements of the velocity derivatives using these new coordinates, can be
written as d3vr d3vx =4ny2dY (4nv2dv). The resulting reaction formula becomes
where K(r,X) = nr(mrl2nkT)3I2nx(mx/2nkT)3/2 .
The second of the two integrals can be written in terms of energy through the
equations E =Ih mv2 and dE =mvdv so v =.J2E / m and dv =dE / .J2mE .
Upon substitution, the second integral becomes
Setting a =~ in the first integral, one obtains fe-av2V2dV. Making a change2kT 0
of variable where f =aV 2, so V = ~ and dV = db, then the first integralV-;; 2vaf
1 =f -~ r.i j: _ reV 2)becomes-m e vsd~ - 3/2' or
2a 0 2a
.J1i (2kT)3/2
2 M 3/ 2
Multiplying the two solutions (ex) and (~) gives
134
(ex).
~( )
3/2=1r 2kT fe-ElkT E1/ 2avdE.2 mM 0
Returning now to the equation for the reaction rate, we find
becomes
R =n n =f ~ 1 e-ElkT El/2avdErX r X 0 V-;- (kT)3/2
Letting I(E) ~ ~2 1,,, e-mTE'''dE, the reaction rate cao be written1r (kT)
=
RrX =nrnx(av) where the reaction probability is (av)= ff(E)avdE whoseo
physical meaning is described as the average probability for a pair of particles in a
cubic centimeter to participate in a nuclear reaction.
The energy generation rate, c, defined as the energy generated by one
gram of stellar matter in one second can be written in ergs/gls as
For two identical nuclei interacting, then r =X and nr nx =nr(nr - 1)/2::::: nr2/2, so
n.n· ( )the reaction rate formula can be rewritten as Rij =-'_J_ av where Oij is a. 1+ c:5jj
Kronecker delta. Since, ni = pNAXi the energy generation equation becomes
135
The product crv is equal to the product of the probability of tunneling
through the Coulomb barrier and the probability of the nuclei engaging in a
nuclear reaction, crv = Pp PN • For a non-resonant reaction the cross section
probability, SeE), is just a constant, so PN =So while the probability for quantum
mechanical tunneling is given by Pp = f-fE-1I2e-b/./E where b represents the
where the reaction probability decreases with increasing charge and for
decreasing energy or temperature.
Substituting the product into the reaction probability formula gives
~ 2f-f 1 ~(av) = ff(E)OVdE =So r= - 3/2 fexp[-EI kT -blJE]dE.o ~n m~T) 0
Obviously, when the term in the exponent is equal to zero, the reaction probability
will be a maximum. In other words, when E/kT + b/-VE is a minimum then the
integrand will be a maximum, i.e., ..!!-(.£+ ~J =O. When this condition isdE kT ~E
( )
2/3
satisfied, the result is l/kT - (b12)E-3/2 =0 so E3
/2 =(bkT12), or Emax = b~T
This form of the equation provides an order of magnitude approximation of the
energy associated with the Gamow peak which describes the optimum value for
136
the energy of the particles that participate in the nuclear energy generating
processes in the Sun. For the p + p reaction, b; ~m; (41<'e' I he0) ;
(27 J1I2 ( 38 2J1.67xlO- kg (39.5)(2.56xlO- C =4.87xlO-6~m/ s and so
2 (8.85xlO-12 C 2/ Nm 2 vAg
( J2/3
_ (bkT)2/3 _ (4.87xlO-6.[kim/ s)(1.38xlO-23 J / K)(1.57x107K)Emax - - ,so
2 2
Emax =(5.28xlO-22)o.6667 =6.52 X 10-15 J:::: 40 keY. This value has the same order
of magnitude as that given by Schwarzschild earlier of 20 keV. A better
approximation can be obtained by transforming the exponential term at the top of
the page into the form of a Gaussian. The width of the Gamow peak can also be
4£5/4derived, where it is found to be Llli = ;;x [ref. 66, p. 161].
v3b
Finally, to put the nuclear energy generation equation into a slightly more
explicit form, the values for NA =6.022 X 1023 and Q (MeV) into units of ergs, Q
=(106 eV)(1.602xlO-19 J/eV)(107 ergs/J) =1.6 x 10-7 ergs give
The final form for the nuclear reaction rate for the p + P step can be written as
has the distinctive T 2/3 and Tl/3 temperature dependences mentioned earlier and
requires extra terms to approximate the non-gaussian shape of the Gamow peak.
137
ApPENDIXC
Solution of the neutrino eigenvalue problem
Written in the form of an eigenvalue equation, the Schrodinger equation
has nontrivial solutions when
det(H f (t) - Li(f)) =0
where the matter modified Hamiltonian in the flavor basis is
1 [- ~ cos 28 + A ~ sin 28JH - 2 2
f -- ~ ~ .2£ -sin 28 -cos28
2 2
Thus, the determinantal equation takes the form
~ 1--cos28+-A-A
4£ 2£
~sin284£
~sin284£ =0~
-cos28-A4£
so (-~COS28+~A-A)(~COS28-A)-(~sin28)2 =04£ 4£ 4£ 4£
and the corresponding quadratic secular equation is
with solutions is
A=~±_1_~A2-2A~cos28+(~cos28Y+(~sin28Y4£ 4£
138
APPENDIXD
Transform of the neutrino vacuum propagation equation
In the basis of mass eigenstates, the evolution equation for the case of
vacuum oscillations can be written in the form of the Schrodinger-like equation
.d Hl-lf/ = If/dt m m
(
VI (t)Jwhere If/m represents the Dirac spinor If/m = .
v2 (t)To obtain the equation
expressing the neutrino evolution in the flavor basis, a unitary transformation is
made using
H'=UHU+
where the neutrino mixing matrix is given by
U =(cos 8 - sin 8Jsin8 cos8
and 8 is the vacuum mixing angle. The Hamiltonian, H, defined through the
equation
becomes
+ (cos 8 - sin 8J M 2 ( cos 8 sin 8JH'=UHU = -sin8 cos8 2p -sin8 cos8
139
=_1(COS a - sin oJ(mt2
2p sin a cos a 0
1 (m12 cos 2 a+ m~ sin 2 a
= 2p (m12
- m~ )sin acos a
The first diagonal term can be expanded as
o )( cos a sin OJm~ -sinO cosO
(m{ - m~ )sin ocos 0)2 2 2 2 •
m1 sin 0+ m2 cos a
m12 cos 2 a+ m~ sin 2 a=.!. (m1
2 cos 2 a+ m12 cos 2 a+ m~ sin 2 a+ m~ sin 2 0)
2
and rewritten as
=~ {m.' eo,'l1+ m,' ,in 2 (} +m; co,' (} +m; ,in 2 (} +m; ,in' (})+ ( m; ; m,' )'in' (} - co,' (})
and similarly for the second diagonal term, m{ sin 2 0+ m~ cos 2 O. Using the
notation ~ =m~ - m~ for the square of the neutrino mass difference, the first
diagonal term now takes the form
(m12
+ m~ Xcos 2 a+ sin 2 0) ~ (. 2 a 2 a) (m~ + mn ~ (. 2 a 2 a)-'--"---..;;...:..."'--------!.. + - sm - cos = + - sm - cos
2 2 2 2
so the transformed Hamiltonian is given by
[
(m2
+m2
) ~(. ) (). ]1 1 2 +- sm 2 0-cos 2 a m12-m~ smocoso
H'=- 2 22 . m2 +m 2
~ .'P (m,' - m;)'10 (}eo,(} ( '2 ,) +2(co,,(} - '10' (})
or H'= m{ +m~ (1 0J+~(-COS20 sin20J.4pOI 4p sin 20 cos 20
140
ApPENDIXE
Transform of the neutrino matter propagation equation
Beginning with the Schrodinger-like equation (since \If represents a Dirac
spinor, IfIj = (~:), and not a wavefunction)
where Ifff represents the state vector in the flavor basis and
1[- ~cos2B+ A ~ Sin2BJH - 2 2
f -- ~ ~ ,2£ -sinZB -cosZB
2 2
Acting on the interaction evolution equation with the mixing matrix in matter
from the left, and using H f =UM HU~ to transform the matrix into the diagonal
basis leads to
Since U~UM =1 and .!!:- (UMiff) =UM dIff + Iff dUM, the above can be written asdt dt dt
'u dlff -(U H ,dUM)1 -- -1-- Iff 'Mdt M dt
Now, acting with U~ from the left and using the unitarity property gives
141
.dlf/ -(H ·U+ dUM)1-- -1 -- If/.dt M dt
The second term on the right hand side can be written explicitly as
+ dUM (coseMU --=M dt -sin eM
where the time derivative acting on UM via the chain rule, i.e.,
d .-cos eM (t) =-sin eM (t)eM ' sodt
and
+ dUM _ . (coseMuM---eMdt -sin eM
-coseMJ.-sin eM
Multiplication of the two matrices gives
(- cos eM sin eM +sin eM cos eM
sin 2 eM +cos 2 eM- cos
2eM - sin 2 eM J (0 -olJ
sin eM cos eM - cos eM sin eM - 1
so
Thus, in the diagonal basis, the spinor propagation equation (using x =t) becomes
[[
- 2 () • deM J]d 1 m1 x 1--
. dx1-lf/ =- If/dx m 2E -i d:; m~(x) m
where ~ 2 =m;2 •. .
142
FIGURES
Figure 1. Partial, Complete and Maxwell-Boltmann Distributions
f(p)
f(p)
8 _10'5
143
II
I/
//
.Ii/ I
II
Figure 3. Masses of two flavors of neutrinos as a function of density
p
FIG. L The masses of two navors of neutrinos as a function of d.ensity. The curves ne~rly cross atone point. Theelectron-antineutrino mass Vf' is also shown.
(from H.A. Bethe, Phys. Rev. Lett. 56 (1986) 1305)
145
Figure 5. MS triangle
,00 I 1-.-._",~.__,L_,.~_~_~_..L.~..J..,J,,~ -JI-.-.-L--L-L....l.....JLLU
,OJ
-EI
WI\!aOt
I
sin260
FIG. 1. Probabinty-oontour plot for detecting an electronneutrino at the Earth which was produced in the solar interior.
(from Parke Phys. Rev. Lett. 57 (1986) 1275)
147
Figure 6. Partial electron degeneracy in the solar core
-2
-1
- 4 t----'----.a...-----L.~__1
~ -3
1016 1015 1014P[Pal
148
Figure 7. Electron number density difference with and without degeneracy
6
(Y)(
Eu
........LD 4(\J
(
0.--i
X
Q)
z2
0.0 0.1
149
Figure 8. Solar density profile (BP2000)
150
(Y)100
<Eu
.........0'
0::r::~
50
0l--.l---L---l.---L-l_1.-.l--...L.-....J-.-L--l_L--.L--L---l.---L..---I_.l-....J.--....J0.0 0.1 0.2 0.3 0.4
R/Ro
150
Figure 9. Partial electron degeneracy in the solar core.
1.5
+>c(I)
() 1.0L(I)
(L
0.5
0.1 0.2R/Ro
151
0.3 0.4
Figure 11. Comparison of density profiles for two SSMs
140
(Y)(
E.
~ 120o
..c0::::
100
0.02
153
0.04R/Ro
0.06 0.08 0.10
Figure 12. The log of electron density versus solar radius (BP2000)(astro-ph/OO10346)
4
3log(njN.) vs. RIRE)
2 BP2000
~ 0Ill>~
-1
-2
-3
-4 a
Fig. 8.... The e!pctron numher density, fie, versus solar radius for the Standard so]ar model(BP2000). The stl'llight·Jine fit shown in Figurp S is an approximation, Eq. (14), given hy BahmH(1989). EqUlltioll (14) hilS boon used previously in many Ilna]yses of lllllttereffocts Oil solllr neutrino
, propagl1tion. Precise nUlllerir~,j vahle, for lle Ilre available Ilt
154
Figure 14. Gamow peak (experimental)
- »!•.a 1.~S 16...J 1~..j uI
10t.-~ I
&
..~
010
o .......A(&II)• K.._ d .... 11.!I87)• o-n.b...d.L (1971)
- ~A(l9!I8)BIR: N..aII- """""(1998)5......1 NoocWl1it
Fig. 1 Astrophysical factor S(E) for the 3HeeHe,2p)'1Ie reaction
(from R. Bonetti et al., "First Measurement of the 3HeeHe,2p)4He CrossSection down to the Lower Edge of the Solar Gamow Peak,"nucl-exl9902004)
156
Figure 15. Log of electron density versus solar radius (sterile neutrinos) (BP2000)(astra-ph/DO10346)
-4 0 0.1 0.2 0.3 0.4 0.5 0.6 0.' 0.8 0.9R/Re
3
2
-2
-3
log(n.wrne!NA) vs. R/Re
BP2000
Fig. 9.HH The number density, fislerile, of scatterers of sterile neutrinos v'Jrsm solar nuHIl8 for tbeStandard solar model (BP2000). The straight line in Figure [I is given by an equation of the sameform as Eft. (14) excrpt that the coeffident for n~terite/N.4 is 22:J (instead of 245 for nelN'l)'
157
Figure 16. Solar neutrino flux
(From A.B. Balantekin, "Neutrinos in Stochastic Media: From Sun to CoreCollapse Supernovae," hep-ph/Ol09163: Solar Neutrino Flux)
10' ------------,
10Ii, (MeV)
FIG It[ 1. Sobr .uun. Ilul. Th< <ffi6~ .. th< rnJ"'lioa flt' ,''' SllIxIInI Sob. M~I ",.u.: kil by I!l< b1xk hondTht IIld clllrd..uon '.'1111110 ftlnWt II'I',~.. ~bylh<>Ia.'W_ nh<_~i. dw lIlOl1l1orllb<oIWaI ..... Ih<I'f<di<"'"'u "'~SlI\""pI\llxlIl<l~ ,.....~ 111<6_""" tU.t=s, ,,-$(\-1..JlInl8:OJ 11l<'JW""'Sl'-i"'J"Iioddv.lo..1Ia01WIM01 cb;<mdia~~~ l..lmlm<hlIWfmr~ihr "I'<fl..,..j<m1f ",ullaril>1lllllw...~II.:cbihlIllmc~ I "~dilcllh<l<ltIl_ .....~.I<Il.......... ,""h"Oi:II~~ ...~.~I"'s.duQN<w!,.,llhotMloly....L ~lIIIdr
we.!I!R<\<If<body,.I>.'li1)-.a1 tin...1''''1".1 6J:l1f" ....1 """"
158
Figure 17. Neutrino production as a function of radius
IGHeulriDo Production
....... Radhu.
PIG. t. Neut.riao procIucdott at • ftIDotlon of rHi-. The .......tioa of neu.trinOI that oriJiute in eIdt fracdoa or the IOIar radi. :ia (dF1ux/d(R/It(j»))[d(R/Ra)). The ....... Wamrateathe prodbCdon fl'IIction tor '». 'Be, H, and bep DeUtrlJwJs forthe «aDdu'd IOIIt model delcribed ia Sec. V.B and Table XI.
Rev. Mod. Phy&. VOl. la, Ho. 2. AtWI 1_
159
Figure 18. Calculated neutrino spectra
0.1 0.2 0.4 0.6 2 10 20
10 12 1r-,==--rF;";"';;;";::';:;:;;';m-:I~
1811
1010
109
108
~ J01U-
10'
105
a 4
105
~.~.:.;.~.
102
101 O·~.1':""'::::..:.J.:~:c...:JILLJ~r:::.u+:li....:J.:...LL:~~~~..:u;~
NeutrIno energy (MeV)
Figure 17: Calculated Neutrino Spectrafrom <http://borex.lngs.infn.it/aboutlborexinof.html>
160
Figure 19. Temperature dependence on solar neutrino fluxes
(6)
I" 11$.7 1$.1 15.1 .8
log 4>(hep) vs. Tc • ....
j-!j
~
j
13j
"'. Ii,
lS.s 11.1
Tc
..6'
!! '" I 1!
..,.;i.;lJJiir,:....{.,
~:~~~ .. ' .-.. . .
log 4>(7B.) vs. Tc
u-
U~i;C2:--""""":-:3'--'::-"-:-'-'":":-:'~""'::"~'-~I:;;'-;7~";';::";;-""-;;";;'~-;"(6) Tc
,.G.N-
e.ate
r .,[~
C.llc..~ .~
~..['M[
f I , " .0.0..U .U IU(4)
lUL'
"
..
Tc
~
'1..J1
~
.I, ,,' " ,,,,,,,,,,,,,,,,,,,]1$.4 JU 15.1 67 t5.8 J~. "
log 4>("B) vs. Tc
(a)
tui...
"•o.•~
t.l
o.r;....
t~
"UI-
t0.5 t. ,,,! , , I , !
15.1 15.2 11.3
T' ., ., ..~~;w~:'j~ ..~ .,.~ 1
~ ~ • a 1~3 ..J
:1',,,,,,""""""",',,""""'" J1$.2 1$.3 1$.4 11.5 15.1 1$.'1' 1i8 Is.a
F!pre '.2 Temperalure depeade""e or lhe '8 ... pp aelIIrlao BuxesIn figure 6.2•• the logarithm of the calculated"B _rino Bux is shownas a function of central lPmperature for the 1& solar models that werecalculated by Bahcall and l'lrich (1988). for this&c-.the temperature isgiven in units of 10" K and the ftux in units of 10'em-· .-'. In Figure 6.2b.the logarithm of the pp neutrino ftux is disp~ .. a function of centraltemperature for the same 1000 solar models. for Ibis figure. the 8ux isexpressed in units of 1010 cm-2 5-1: the unit oI'&emperature is the sameas for figure 6.20
r_ U Tempenlure depeBdell<e of lhe bep _ T.Be _.rino 8""esIn figure 6.3a. the Iogarithm of the calculated hop neumno 8ux IS shown as• function of central temperattUe for the 1000 solar models that. were cal-culated b,' Bahcall and l'\rich (1988). In figure 6.36. lhe logarithm of theTae Df'utrlno 8ux is displayed as a (unction of central temperature for thesame 1000 solar models. The unit of temperature is 10' K. for figure 6.3a.the fluxes are expressed in units of loJ cm-t S-I and for Figure 6.36. inunits of lOS' cm-2 5- 1•
161
Figure 20. Level crossing diagram for SN neutrinos
normal hierarchy
v'f
ne
L-resonance
mI-V_3 -+~.....---V~(I;l
E~U V2
~
vacuum SN core
Figure 2. Level crossing diagram for normal mass hierarchies(from Takahashi and Sato, Prog. Theor. Phys. 109 (2003) 921)
162
Figure 21. Pre-SN density profile for 15 Mo star
H
10.1radius(sofar radius)
O+C HeO+Ne+Mg1x106r---........--.........-----+-----.
lOOO(l(l
10000
1000iQ 100
i 1~v
0.1
0.010.001""- .....
0.01
FIG. 3. Density profile of the presupemova star model used inthe paper [20]. The progenitor mass is set to be 15M0 .
(from Takahashi et aI., Phys. Rev. D 64 (2001) 093004 where ref. 20 isS.B. Woosley and T.A. Weaver, Ap. J. SuppI. 101 (1995) 181)
163
Figure 22. Evolution of neutrinos with different energies
--------_._._---------
-----..---.~.......-.....""'--.....
.---_.....-_ .._-_ .._----------_.
"
Figure 9: The !!I'olutioll of tllP l!eutrinn-; with dill'enmt, PIlergies in the Sun, Shown arethe dep()IHlenGes of the ilveillged value of the surviv1u prob'lbility (dashed lines), as well asInaxinml Hnd mininml values of the probability (solid lines) OIl n. Neutrino is produced illtho center of th,) SUll. The density df1creases from the loft to the right. The rOSOIlaJlce eisat n = O. The probability is the oBl:illatory curve which is iliS< Tibed in the band betweenpmux and pmi". Upper left pallel: E 14;\leV, upper right panel: E fi l\JeV, lower leftpimP] E = 2 !vleV, lower right panel E= O.8(j MeV.
(from Smimov hep-ph/0305106)
164
Figure 23. Survival probabilities
Figure f): The dependl~nCt~ of the average probability (dashed line) and the depth ofoscillations (IJ""'X, pm;n solid lines) OIl n for no = --5. The reSOIlHnee layer corresponds to11. O. For tan2 (/ "'. 0.4 (large mixjn~; MSW solution) the evolution stops at 11, '" 0.47.
165
Figure 24. Profile of survival probabilities
..••
• 2
., 1., ,.S
Figure 8: Profile of the effect. Dependence or the surviwd proof\bility on nentrino energyfor the best fit values of parameters and production in the center of the Sun (solid line).For tJ.m2 =. 7.10 5 e\'2. x ~= 2 corresponds w E ~ 10 MeV. The dashed line shows theilveraging effeet over the production region R O.1R."". The Earth matter regenerationeffect is not included.
Figure 25. Level-crossing
Figure 3: Level crossing scheme..Dependence of the eigenvalues of the Hamiltonian inIllatter, HIm lutd H2rn , on the ratio x == lv/lo for t\VO different values of VRenUIn Inixingsin2 20 =···0.825 (solid, blue lines) and sin2 0=· O.OS (dashed, red lines).
166
Figure 26. MSW Contour Plot
1r &.1 G2 U U 0.& 0.1 U 0.1 0.1 1tit
,''' 0.1 OJ! U OA U U 0.7 U ... 1til
Figure 7: The be,'t fit points and t.he allowed regions (at. different C.L.) of the 06Cillationparameters (at different C.L.) from the global fit of tile solar neutrino data (left), and froIllthe combined analysis of the solar neutrino data and KamLAND (rignt).
(Smimov hep-phl03050106)
167
Figure 27. Electron number densityvs. solar radius (JCD1987)
6.0.1025
5.0.1025
4.0.1025
(Y)<Eu
:::::3.0.1025Q)
z
2.0.1025
1.0.1025
0.0 0.1
168
0.2R/Ro
0.3 0.4
Figure 28. Electron number density vs. solar radius (BP2000)
6.0,1025
5.0.1025
4.0,10 25(Y)
(
Eu
~3.0·1025L:0:::
2.0,1025
1.0.1025
0.0 0.1
169
0.2R/Ro
0.3 0.4
Figure 29. Electron number densities for BP2000 (upper) & JCD1987 (lower)
5.0.1025
4.0.1025
(Y)
~3.0.1025"-~
o.ccr
2.0.1025
1.0.1025
0.050 0.075 0.100
170
0.125R/Ro
0.150 0.175 0.200
Figure 30. Induced mass A vs. sin2 20 M showing matter induced resonance effects
AFIG. 2. Plot of sin220"p where Om's the etfectiveneutrino mixing angle in matter. as a function of A. the induced electronneutrino mass. Here we take mj -m f==3.0 and sin28=0.03.
(from Kuo and Pantaleone Rev. Mod. Phys. 61 (1989) 947)
171
Figure 31. A vs. sin2 28M using LMA parameters where Pc=35 glee & Rc= 0.2 Ro
0.8
EI
10 0.6+.>(l)
..c+.>•(\J
(\J0.4(
c..-i(I)
0.2
0.5
172
1.0A
1.5 2.0
Figure 32. Neutrino level crossing diagram using LMA parameters
2.01.51.0A
0.5
1.25
a.aa L--...L.----'-----'---'-_'--...L.----'-------'---'-_'---'-----'------'----'_-'-----'-------'-----L_L--J
0.0
0.25
1.00
(\J<J.)<n 0.75<n10E
0.50
173
Figure 33. The solar pp chain
2 + 2 .p+p .... H+e +p p+p+e· .... H+p
t_-f-_t99.75% 0.25%
2H + P_JHe +,.86% t 14%t~---_"--:"':'t
\Ie + JHe ...."He +2p JHe + "He ....7& +.,
t 0.11%
t7Be + p ....HB +-r
t3n .....Rae· +e+ +.,
ppl ppll ppIlI
I From Balantekin and Haxton, "Solar, Supernova and Atmospheric Neutrinos,"nucl-th/9903038.
174
Figure 34. Degenerate density vs. exponential density profiles
150
100(Y)
:>- (
.j...> E..... uII)
c '-(J) ~
0 0...c.0::::
50
ol-.L-----L--L----l-~:L----L--l.----L-~"f___~::::L:::±:~=:l::::==!=o 1.0.108 2.0.108 3.0.108 4.0.10 8
R A = 245 alpha = 10.54
175
Figure 35. Degenerate vs. nondegenerate exponential profiles
150
100
50
oL-..L.---l..-..J--rf--L-....I---L--.L~:::::~~=~:=..Jo 1.0.108 2.0.108 3.0.108 4.0.108
R
176
Figure 36. Evolution of P(ve~ ve) using incorrect mixing matrix
0.8
0.6:>1\II
:>
0....
0.4
0.2
0.2 0.4R/Ro
177
0.6E= 10 MeV
0.8 1.0
Figure 37. Evolution of P(ve~ ve) using corrected mixing matrix
1.0
0.8
~ 0.6II::>
Q...
0.4
0.2
0.2 0.4R/Ro
178
0.6 0.8E= 10 MeV
1.0
Figure 38. Evolution of P(ve ---7 ve) using JeD SSM (Degenerate case) Step = 1
1.0
:>1\II
:>
a...
0.8
0.6
0.4
0.2
0.2R/Ro
0.4 0.6 0.8 1.0E = 10 MeV --> sdens=rho(1+Xl/2
179
Figure 39. Evolution of P(ve~ ve) using JeD SSM (Nondegen case) Step =1
1.0
0.8
> 0.61\
II
>0.-
0.4
0.2
0.2R/Ro
0.4 0.6 0.8 1.0E = 10 MeV n) sdens=rho(l+XJ/2
180
Figure 40. Percent difference in P(ve -7 ve) using JeD SSM (Step = 1)
100
> 50/\,,>
CLICJ+->......Q)
0~
0
-50
0.0 0.2R/Ro
0.4E= 10 MeV
181
0.6 0.8-->sdens=rholl + Xl/2
1.0
Figure 41. Evolution of P(ve~ ve) using JeD SSM (Degenerate case) Step =lh
1.0
0.8
::>- 0.6/\II
::>-
0.-- 0.4
0.2 0.4 0.6 0.8 1.0E = 10 MeV --) sdens=rhofl >XJ/2 >LIN.INTERp·
0.2
o.0 '-----J----I.-..L-L.....L.......L-.L.....J----I.-..L-L.....L.......L-.l.-JL....L-..L---l-.....L.......L-.L.....JL....L-..L--L---l.--LJ
0.0R/Ro
182
Figure 42. Evolution of P(ve -7 ve) using JeD SSM (Nondegen case) Step =Y2
1.0
0.8
> 0.6/\II
>0....
0.4
0.2
o.0 L-L---'---L......L-L.-.L---'---L......L-L....L-L--L-..L-Jl-L-L--L-..L-L..L~..-I---l.-L...1-LJ
0.0 0.2 0.4 0.6 0.8 1.0R/Ro E = 10 MeV --> sdens=rhoO' Xl/2 ·UN.INTERP-
183
Figure 43. Percent difference in P(ve --7 ve) using JeD SSM (Step =1)
100
:>- 501\II
:>-(L
10+-'
Q)
0~
0
-50
0.0R/Ro
0.2 0.4 0.6 0.8 1.0E= 10 MeV u)sdens=rhoC1+X)/2 LIN.INTERP-
184
Figure 44. Electron neutrino survival probability for Ev = 14 MeV
1.0
-1 0E = 14 MeV
>1\I.>
Q...
0.8
0.6
0.4
0.2
o.0 ~--.L---l....-L---l-....L-.l..--l.--.I--1.--L-.L-..l.--L-..l.-.L.-JL...-L--L........l-L-L........L-~
-5 -4 -3 -2NegatIve DensIty/DensIty at Resonance
185
Figure 45. Electron neutrino survival probability for Ev = 6 MeV
1.0
>1\
I,>
0...
0.8
0.6
0.4
0.2
-1 0E = 6 MeV
o.0 ~'--'---'----L.----'---'---'--....l...--'--.l..--L--J-.l---L--L---L-L.--'--....L-...L-...l.....-.l..--L--Jl...-.i
-5 -4 -3 -2NegatIve DensIty/DensIty at Resonance
186
Figure 46. Electron neutrino survival probability for Ev =2 MeV
1.0
:>/\II
:>
0...
0.8
0.6
0.4
0.2
-1 0E = 2 MeV
o.0 ::--,-.-L-..L--.L---L-...L-L-.J.-L-L--.L---L-...L-.L-1--L---L.--.L-....L.......l--L-.J.-L---L..J
-5 -4 -3 -2NegatIve DensIty/DensIty at Resonance
187
Figure 47. Electron neutrino survival probability for Ev=O.86 MeV
1.0
>/\II
>(L
0.8
0.6
0.4
0.2
-1 0E = 0.86 MeV
o.0 L-.J'---.l.-----L.........L-L-L-l.---L.-...L-L-l.---l-----l.---L-L-L-L.--l.---L.-...l.-...L-.L-L-...JL...J
-5 -4 -3 -2NegatIve DensIty/DensIty at Resonance
188
Figure 48. Interpolated ratio of FD integrals
1.5
oLL
1.0
0.5
0.0 0.1R/Ro
189
0.3E= 10 MeV
0.4-->F'erm12.F'
0.5
Figure 49. Evolution of P(ve --7 ve) using BP SSM (Degenerate case) Step =1
1.0
0.8
> 0.6I,>
0...
0.4
0.2
0.2 0.4R/Ro
190
0.6 0.8E ; 10 MeV
1.0
Figure 50. Evolution of P(ve ~ ve) using BP SSM (Nondegen case) Step = 1
1.0
0.8
7' 0.6,>
(L
0.4
0.2
0.2 0.4R/Ro
191
0.6 0.8E = 10 MeV
1.0
Figure 51. Percent difference in P(ve~ ve) using BP SSM (Step =1)
50
:>1\,I
:>
0... 0iO+>.......Q)
0~
-50
0.2 0.4R/Ro
192
0.6E= 10 MeV
0.8 1.0
Figure 52. Evolution of P(ve~ ve) using BP SSM (Nondegen case) 8 12 =33°
1.00.6 0.8E = 10 MeV
0.4R/Ro
0.2
1.0
o.0 '----'---'---L-l--L-..l.-L-.1----1...---l---L.....l-.L-L-.1----1...---l---L.....l-.L-L-.J.----I...---l---L..-L-..J....;
0.0
0.8
0.4
0.2
~ 0.6I,:>-
0...
193
Figure 53. Evolution of P(ve -7 ve) using BP SSM (Degenerate case) 812 =33°
1.0
:>f\,,:>
0-.
0.8
0.6
0.4
0.2
0.4
194
0.6R/Ro
0.8 1.0
Figure 54. Percent difference in P(ve -7 ve) using BP SSM (812 =33°)
100
::./\ 50,,::.
Cl.-
IO+.>-<(I) 00~
-50
-10 0 L-Jl-....1----L.........L---L--L----L--L.--L.....L......L........L....-.L..-.l....-.L-l-L-.J------.l---'------'----'---.L-..L........J
0.0 0.2 0.4 0.6 0.8 1.0R/Ro E= 10 MeV
195
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