excerpt from, analyzing convective heat transfer
TRANSCRIPT
__________________________ 1Student, Department of Mechanical Engineering, Clemson, SC 29631
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The following excerpt is from a senior-level mechanical engineering lab report. The experiment and
report was a group assignment; however, I was responsible for the theoretical analysis that is presented
in Section C as well as Appendix A, B and C. I have removed text that was written by my teammates, but
have included the Abstract and Introduction to provide the reader with some background information
about the assignment.
Excerpt From,
“Analyzing Convective Heat Transfer” ME 444
November 2012
Heat transfer analysis has many applications in engineering design, especially where the time necessary to
change an objects temperature is needed. As an example of this analysis, the experiment examined a solid
sphere and cuboid exposed to free and forced convection. The convective heat transfer coefficient and time
required for heat transfer was determined from experimental data for both specimens in each mode of
convection. Theoretical values for these parameters were also determined, and then compared with
experimental results. Two analytical models were used to calculate the theoretical values: the lumped
parameter model and a transient 1-dimensional analysis. Overall, both analytical models appropriately
represented the system, but the results from the transient analysis were most accurate. Uncertainty analysis
and error propagation were conducted to determine the confidence in the reported values.
I. Introduction
HE transfer of heat between a solid object and a fluid is known as convection. Convection is classified
according to the nature of the fluid’s flow. Forced convection is used to describe circumstances when the flow
is caused by an external force, such as a fan or the earth’s atmosphere. Free convection is used to describe situations
when the fluid flow is caused by buoyant forces, which are created by the temperature induced density gradient in
the fluid. Both methods of convection can be analyzed to determine specific properties and parameters of the heat
transfer. One valuable parameter is the convection heat transfer coefficient, which is proportional to the rate of heat
transfer between the solid and the fluid. This coefficient is useful for determining the time required for convection to
raise or lower an object’s temperature and has many practical design applications.
Concepts of convection and the heat transfer coefficient were explored using a metal sphere and cuboid. Each
solid’s temperature was lowered near 0° C, and then exposed to free or forced convection until their temperature
reached steady state (room temperature ~ 23°C). The convection heat transfer coefficient for each solid in each
method of convection was determined from the experimental data. The heat transfer coefficient was also analytically
determined using an appropriate thermal model, and these values were compared. Similar thermal analysis can be
T
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applied to similarly shaped objects such as coolers, homes, electrical components, or vehicles. Analysis can
determine the time required for liquid in a cooler to become warm, a home to warm up at night, or time for a
computer or engine to overheat in given conditions.
[…text removed…]
C. Analysis Procedure
1. Lumped Parameter Model
The average convection heat transfer coefficient for each solid in each method of convection was analytically
determined to validate experimental data. The lumped parameter model was used for this analysis. This model
assumes that the temperature of the solid is uniform at any instant in time during the heat transfer process1.
Essentially, this model neglects any temperature gradient within the solid and allows the temperature measured by
the thermocouple to represent the temperature of the entire solid.
The following condition was used to verify that the lumped parameter model provided reasonable results:
(1)
where h is the heat transfer coefficient, Lc is the characteristic length, k is the fluid’s thermal conductivity, and Bi is
the Biot number. The Biot number represents the measure of temperature drop within a solid relative to the
temperature difference between the solid and its surroundings1. For the circumstances in this analysis, the Biot
number was approximately 0.012; therefore, the error created by the lumped parameter model was small and the
model was appropriate to use.
a.) Free Convection - Theoretical Heat Transfer Coefficient
The following assumptions were made before applying the lumped parameter model to each solid in free
convection:
1. The solids’ surface is isothermal
2. Thermal effects due to radiation are negligible
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3. The solid is made of stainless steel (AISI 304)
4. The surrounding air is quiescent
The average heat transfer coefficient of a solid in free convection is dependent upon several
dimensionless parameters. These parameters are shown in Table 2 (see Appendix A for each expression’s
conditions). The average convective heat transfer coefficient was then found using the following
relationship:
(2)
where h is the heat transfer coefficient, L is the characteristic length, k is the fluid’s thermal conductivity,
and Nu is the Nusselt number (a dimensionless parameter).
Table 2 Dimensionless Parameters for Free Convection
N
o
t
i
c
e
Notice that three different Nusselt numbers were needed to model the cuboid. Different expressions were
needed because the surfaces of the cube do not experience the same heat transfer because of their orientation
relative to buoyant forces (gravity). Therefore, each surface had an individual heat transfer coefficient, and
these values were combined using the following expression to determine the average heat transfer coefficient
for the entire solid:
( ) ( ) ( )
( ) (3)
Sphere Cuboid
Rayleigh
Number
RaD g Ti T D3
Nusselt
Number
NuD 20.589RaD
1/4
1 0.469/Pr 9/1 6
4 /9
RaL g Ti T L3
Nutop 0.27RaL1/4
Nubottom 0.15RaL1/3
Nuside 0.680.670RaL
1/ 4
1 0.492/Pr 9 /16
4 / 9
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b.) Forced Convection – Theoretical Heat Transfer Coefficient
The analysis for each solid in forced convection was similar to the free convection analysis; however, the
Rayleigh number was replaced with the flow’s Reynolds number. The equations used to calculate the
average heat transfer coefficient for the sphere and cuboid in forced convection is shown in Table 3 (see
Appendix A for each expression’s conditions).
Table 3 Dimensionless Parameters for Forced Convection
T
h
e front and back surfaces of the cuboid in forced convection were modeled as surfaces in free convection.
This was appropriate because these surfaces are oriented perpendicular to the fluid’s flow; therefore, the
fluid is stagnant at these surfaces and no forced convection takes place. The parameters in Table 3 show the
equations for the remaining four surfaces that were parallel to the fluid flow.
The average heat transfer coefficient for each solid was determined using the same relationships for
that were shown for free convection.
Also, the following assumptions were used during forced convection analysis:
1. The solid’s surface is isothermal
2. Thermal effects due to radiation are negligible
3. The solid is made of stainless steel (AISI 304)
c.) Time Required for Heat Transfer
The time required to heat each solid to room temperature was determined by using the following
equation:
(
) (4)
Sphere Cuboid
Reynolds
Number
ReVD
ReVD
Nusselt
Number
NuD 2 0.4ReD1/ 20.06ReD
2 / 3 Pr0.4
film
NuD 0.644Re1/2Pr1/3
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where ρ and Cp are material properties evaluated at room temperature, A is the solid’s surface area, and is
the solid’s volume. Details for the calculations are given in Appendix A.
2. Experimental Analysis
Analyzing the experimental data, heat transfer coefficients for each scenario were found based on initial and
final temperatures of the specimen, ambient air temperature, and time for the temperature change. Using these
values and manipulating Eq. 4, an overall heat transfer coefficient was found from the actual data. The temperature
curves using the calculated theoretical coefficients and the empirical coefficients were compared and can be seen in
Section III. Details for the calculations are given in Appendix B.
3. Transient 1-Dimensional Heat Transfer
Although it was shown that the lumped parameter model provides appropriate results, the sphere in free
convection was also analyzed with a transient internal temperature distribution. This additional analysis is a more
complicated alternative to the lumped parameter model, but is regarded as a more accurate analysis. The cuboid was
not analyzed because of its more complicated geometry.
Transient 1-dimensional analysis was used to determine the average convective heat transfer coefficient that
provided a cooling time most similar to the experimental cooling time. The coefficient was then used to validate
other analytical and experimental results. The cooling time for transient analysis is shown in Equation (5), where Fo
is the dimensionless Fourier number, ro is the sphere’s radius, and α is the metal’s thermal diffusivity.
(5)
The Fourier number is expressed by the following equation, where ζ and C1 are tabulated values that rely on the heat
transfer coefficient:
[
] (6)
Details for the calculations are given in Appendix C.
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Appendix A
Theoretical heat transfer analysis.
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%% Measured Temperatures
Tinf = 296; % K (room temperature)
Ti = 273; % K (initial surface temperature)
Tf = 284.5; % K (film temperature = (Ti+Tinf)/2))
Tfinal = 291.5;
% Tfinal = Tinf-0.02*Tinf % K (Threshold for steady state temp.)
%% Test Specimen Dimensions
Ds = 0.0381; % m (sphere diameter)
Vol = 0.0254*0.02536*0.02536; % m^3 (Volume of cube)
At = 0.00064313; % m^2 (surface area of top & bottom surfaces of cube)
As = 0.00064414; % m^2 (surface area of side of cube)
Ac = (4*As)+At+At; % m^2 (surface area of entire cube)
Per = 0.1014; % m (perimeter of top & bottom surfaces of cube)
Ltb = At/Per; % m (charac. length of top & bottom surfaces of cube)
Ls = 0.0254; % m (charac. length of vertical side of cube)
Ls_perp = 0.02536; % m (charac. length of side in forced convec.)
%% Metal Properties at 300K
% Stainless Steel (AISI 304) (Table A.1 Incropera)
den_ss = 7900; % kg/m^3
Cp_ss = 477; % J/kgK
k_ss = 14.9; % W/mK
%% Air Properties
% Air at Room Temperature (Tinf = 296K)
mu_inf = 0.00001826; % Ns/m^2
nu_inf = 0.00001553; % m^2/s
k_inf = 0.0257; % W/mK
Pr_inf = 0.708;
% Air at Film Temperature (Tf = (Ti + Tinf)/2 = 284.5K)
mu_f = 0.00001769; % Ns/m^2
nu_f = 0.00001451; % m^2/s
k_f = 0.0251; % W/mk
alpha_f = 0.00002045; % m^2/s
Pr_f = 0.716;
%% Experimental Constants
g = 9.81; % m/s^2
V = 2.8; % m/s (air speed)
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%% Sphere in Free Convections
Ra_sfree = abs((g*(1/Tinf)*(Ti-Tinf)*(Ds^3))/(alpha_f*nu_f));
Nu_sfree = 2 + (0.589*(Ra_sfree^0.25))/(1 + (0.469/Pr_f)^(9/16))^(4/9);
h_sfree = Nu_sfree*(k_f/Ds)
%% Sphere in Forced Convection
Re_sforc = V*Ds/nu_inf;
Nu_sforc = 2 + (0.4*sqrt(Re_sforc) +
0.06*Re_sforc^(2/3))*(Pr_inf^0.4)*(mu_inf/mu_f);
h_sforc = Nu_sforc*(k_inf/Ds)
%% Cuboid in Free Convection
% Top Surface
Ra_top_fre = abs((g*(1/Tinf)*(Ti-Tinf)*(Ltb^3))/(alpha_f*nu_f));
Nu_top_fre = 0.27*(Ra_top_fre^.25);
h_top_fre = Nu_top_fre*(k_f/Ltb);
% Bottom Surface
Ra_bott_fre = Ra_top_fre;
Nu_bott_fre = 0.15*(Ra_bott_fre^(1/3));
h_bott_fre = Nu_bott_fre*(k_f/Ltb);
% Side Surface
Ra_Csfree = abs((g*(1/Tinf)*(Ti-Tinf)*(Ls^3))/(alpha_f*nu_f));
Nu_Csfree = 0.68 + (0.670*(Ra_Csfree^0.25))/(1 + (0.469/Pr_f)^(9/16))^(4/9);
h_Csfree = Nu_Csfree*(k_f/Ls);
% Total Area
h_cfree = ((4*h_Csfree*As)+(h_top_fre*At)+(h_bott_fre*At))/(4*As + At + At)
%% Cuboid in Forced Convection
% Surfaces parallel with flow direction
Re_CPforc = V*Ls_perp/nu_inf;
Nu_CPforc = 0.664*sqrt(Re_CPforc)*(Pr_inf^(1/3));
h_CPforc = Nu_CPforc*k_f/Ls_perp;
% Surfaces perpindicular to flow direction (modeled as free convection)
h_CPerforc = h_Csfree;
% Total Area
h_cforc = (2*As*h_CPerforc + (2*As+2*At)*h_CPforc)/(4*As + 2*At)
%% Time to reach steady state
% Free Sphere
t_sfree = ((den_ss*Cp_ss*Ds)/(h_sfree*6))*log((Ti-Tinf)/(Tfinal-Tinf))/60
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% Forced Sphere
t_sforc = ((den_ss*Cp_ss*Ds)/(h_sforc*6))*log((Ti-Tinf)/(Tfinal-Tinf))/60
% Free Cube
t_cfree = ((den_ss*Cp_ss*Vol)/(Ac*h_cfree))*log((Ti-Tinf)/(Tfinal-Tinf))/60
% Forced Cube
t_cforc = ((den_ss*Cp_ss*Vol)/((2*At+2*As)*h_CPforc))*log((Ti-Tinf)/(Tfinal-
Tinf))/60
Appendix B
Experimental heat transfer analysis.
%Free Sphere % Define constants
% Stainless Steel AISI 304 at 300K (from Table A.1) den = 7769.8; % kg/m^3 Cp = 477; % J/kgK
% Sample Diameter D = 0.0381; % meter
Ti = 273; % Specimen's initial temp [K] Tinf = 296; % Temp of Ambient Air [K]
%Theoretical hbar hbar = 7.585; % Define relationship between Temperature (T) and time (t) t = 0:0.5:5400; % time [0-90min every 0.5 second] T = Tinf+((Ti-Tinf)*exp((-6*hbar*t)/(den*Cp*D)))-273; % Specimen's Temp [K]
% Plot Sample's Temperature with respect to time figure(1) hold on plot(t,T,'--r')
%Experimental hbar %Define experimental parameters Texp = 291.4; %Final experimental temperature texp = 4000; %Total experimental time
%Solve for experimental hbar hbar_exp = den*Cp*D*log((Ti-Tinf)/(Texp-Tinf))/(6*texp);
% Define relationship between Temperature (T) and time (t) texp = 0:0.5:5400; % time [0-90min every 0.5 second] Texp = Tinf+((Ti-Tinf)*exp((-6*hbar_exp*t)/(den*Cp*D)))-273; % Specimen's
Temp [K]
plot(texp,Texp,'--b')
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%Plot Experimental Data plot(frstime,frstemp)
%Theoretical Dry Curve %Define dry parameters Tdry = 291.4; %Final experimental temperature tdry = 1200; %Total dry curve time Tidry = 289.5; %Start of dry curve
%Solve for experimental hbar hbar_dry = den*Cp*D*log((Tidry-Tinf)/(Tdry-Tinf))/(6*tdry);
% Define relationship between Temperature (T) and time (t) tdry = 0:0.5:5400; % time [0-90min every 0.5 second] Tdry = Tinf+((Ti-Tinf)*exp((-6*hbar_dry*t)/(den*Cp*D)))-273; % Specimen's
Temp [K]
plot(tdry,Tdry,'--g')
%Free Cube % Define constants
% Stainless Steel AISI 304 at 300K (from Table A.1) den = 7284.8; % kg/m^3 Cp = 477; % J/kgK
% Sample Dimensions Vol = 0.0254*0.02536*0.02536; % m^3 (Volume of cube) At = 0.00064313; % m^2 (surface area of top & bottom surfaces of cube) As = 0.00064414; % m^2 (surface area of side of cube) Ac = (4*As)+At+At; % m^2 (surface area of entire cube)
Ti = 273; % Specimen's initial temp [K] Tinf = 296; % Temp of Ambient Air [K]
%Theoretical hbar hbar = 7.16; % Define relationship between Temperature (T) and time (t) t = 0:0.5:5400; % time [0-90min every 0.5 second] T = Tinf+((Ti-Tinf)*exp((-Ac*hbar*t)/(den*Cp*Vol)))-273; % Specimen's Temp
[K]
% Plot Sample's Temperature with respect to time figure(1) hold on plot(t,T,'--r')
%Experimental hbar %Define experimental parameters Texp = 293.4; %Final experimental temperature texp = 4200; %Total experimental time
%Solve for experimental hbar
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hbar_exp = den*Cp*Vol*log((Ti-Tinf)/(Texp-Tinf))/(Ac*texp);
% Define relationship between Temperature (T) and time (t) texp = 0:0.5:5400; % time [0-90min every 0.5 second] Texp = Tinf+((Ti-Tinf)*exp((-Ac*hbar_exp*t)/(den*Cp*Vol)))-273; % Specimen's
Temp [K]
plot(texp,Texp,'--b')
%Plot Experimental Data plot(frctime,frctemp)
%Theoretical Dry Curve %Define dry parameters Tdry = 293.4; %Final experimental temperature tdry = 2150; %Total dry curve time Tidry = 290; %Start of dry curve
%Solve for experimental hbar hbar_dry = den*Cp*Vol*log((Tidry-Tinf)/(Tdry-Tinf))/(Ac*tdry);
% Define relationship between Temperature (T) and time (t) tdry = 0:0.5:5400; % time [0-90min every 0.5 second] Tdry = Tinf+((Ti-Tinf)*exp((-Ac*hbar_dry*t)/(den*Cp*Vol)))-273; % Specimen's
Temp [K]
plot(tdry,Tdry,'--g')
%Forced Sphere % Define constants
% Stainless Steel AISI 304 at 300K (from Table A.1) den = 7769.8; % kg/m^3 Cp = 477; % J/kgK
% Sample Diameter D = 0.0381; % meter
Ti = 273; % Specimen's initial temp [K] Tinf = 296; % Temp of Ambient Air [K]
%Theoretical hbar hbar = 34.6; % Define relationship between Temperature (T) and time (t) t = 0:0.5:3500; % time [0-90min every 0.5 second] T = Tinf+((Ti-Tinf)*exp((-6*hbar*t)/(den*Cp*D)))-273; % Specimen's Temp [K]
% Plot Sample's Temperature with respect to time figure(1) hold on plot(t,T,'--r')
%Experimental hbar
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%Define experimental parameters Texp = 294.5; %Final experimental temperature texp = 2300; %Total experimental time
%Solve for experimental hbar hbar_exp = den*Cp*D*log((Ti-Tinf)/(Texp-Tinf))/(6*texp);
% Define relationship between Temperature (T) and time (t) texp = 0:0.5:3500; % time [0-90min every 0.5 second] Texp = Tinf+((Ti-Tinf)*exp((-6*hbar_exp*t)/(den*Cp*D)))-273; % Specimen's
Temp [K]
plot(texp,Texp,'--b')
%Plot Experimental Data plot(fostime,fostemp)
%Forced Cube % Define constants
% Stainless Steel AISI 304 at 300K (from Table A.1) den = 7284.8; % kg/m^3 Cp = 477; % J/kgK
% Sample Dimensions Vol = 0.0254*0.02536*0.02536; % m^3 (Volume of cube) At = 0.00064313; % m^2 (surface area of top & bottom surfaces of cube) As = 0.00064414; % m^2 (surface area of side of cube) Ac = (4*As)+At+At; % m^2 (surface area of entire cube)
Ti = 273; % Specimen's initial temp [K] Tinf = 296; % Temp of Ambient Air [K]
%Theoretical hbar hbar = 29.09; % Define relationship between Temperature (T) and time (t) t = 0:0.5:3500; % time [0-90min every 0.5 second] T = Tinf+((Ti-Tinf)*exp((-Ac*hbar*t)/(den*Cp*Vol)))-273; % Specimen's Temp
[K]
% Plot Sample's Temperature with respect to time figure(1) hold on plot(t,T,'--r')
%Experimental hbar %Define experimental parameters Texp = 294.5; %Final experimental temperature texp = 1800; %Total experimental time
%Solve for experimental hbar hbar_exp = den*Cp*Vol*log((Ti-Tinf)/(Texp-Tinf))/(Ac*texp);
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% Define relationship between Temperature (T) and time (t) texp = 0:0.5:3500; % time [0-90min every 0.5 second] Texp = Tinf+((Ti-Tinf)*exp((-Ac*hbar_exp*t)/(den*Cp*Vol)))-273; % Specimen's
Temp [K]
plot(texp,Texp,'--b')
%Plot Experimental Data plot(foctime,foctemp)
Appendix C
Theoretical analysis using a transient 1-dimensional model.
%% Sphere - Free Convection with transient heat transfer
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%% Metal Properties at 300K
% Stainless Steel (AISI 304) (Table A.1 Incropera)
den_ss = 7900; % kg/m^3
alpha_ss = 0.00000394; % J/kgK
k_ss = 14.9; % W/mK
r = 0.0381/2; % radius (meter)
%% Measured Temperatures
Tinf = 296; % K (room temperature)
Ti = 273; % K (initial surface temperature)
Tf = 284.5; % K (film temperature = (Ti+Tinf)/2))
Tfinal = 291.5;
% Tfinal = Tinf-0.02*Tinf % K (Threshold for steady state temp.)
%% Coefficients for transient 1-Dimensional conduction (h = 9.4, Bi = 0.012)
Bi1 = 0.010;
h1 = Bi1*k_ss/r
z1 = 0.1730; % rad
C1 = 1.0030;
Bi2 = 0.011;
h2 = Bi2*k_ss/r
z2 = 0.1802; % rad
C2 = 1.0033;
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Bi3 = 0.012;
h3 = Bi3*k_ss/r
z3 = 0.1880; % rad
C3 = 1.0036;
Bi4 = 0.013;
h4 = Bi4*k_ss/r
z4 = 0.1945; % rad
C4 = 1.0039;
Bi5 = 0.014;
h5 = Bi5*k_ss/r
z5 = 0.2016; % rad
C5 = 1.0042;
%% Analysis
Fo1 = -(1/(z1^2))*log((1/C1)*((Tfinal-Tinf)/(Ti-Tinf)));
t1 = (r^2)*(Fo1/alpha_ss)/60 % min
Fo2 = -(1/(z2^2))*log((1/C2)*((Tfinal-Tinf)/(Ti-Tinf)));
t2 = (r^2)*(Fo2/alpha_ss)/60 % min
Fo3 = -(1/(z3^2))*log((1/C3)*((Tfinal-Tinf)/(Ti-Tinf)));
t3 = (r^2)*(Fo3/alpha_ss)/60 % min
Fo4 = -(1/(z4^2))*log((1/C4)*((Tfinal-Tinf)/(Ti-Tinf)));
t4 = (r^2)*(Fo4/alpha_ss)/60 % min
Fo5 = -(1/(z5^2))*log((1/C5)*((Tfinal-Tinf)/(Ti-Tinf)));
t5 = (r^2)*(Fo5/alpha_ss)/60 % min
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References
1 Incropera, Frank P., and David P. DeWitt. Fundamentals of Heat and Mass Transfer. New York: Wiley, 1990.
Print. 2
Wagner, J., Ph.D., P.E., and Freeman, T., ME 444 – Mechanical Engineering Lab III Student Manual, Fall 2012,
Clemson University, Clemson, South Carolina, Chap. 2.