chaos and control in combustion steve scott school of chemistry university of leeds

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Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

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Page 1: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Chaos and Controlin Combustion

Steve Scott

School of Chemistry

University of Leeds

Page 2: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Outline

• Review of H2 and CO combustion

• Use of flow reactors

• Oscillatory ignition

• Mechanistic comments

• Complex oscillations

• Chaos

• Control of Chaos

Page 3: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

The H2 + O2 reaction

The classic example of a branched chain reaction

simplest combustion reaction etc.

s lo w re ac tio n

th ird lim it

sec o n dlim it

firs t lim it

ig n itio n

am b ie n t te m p e ra tu re , T /Ka

pres

sure

, p/to

rr4 0 0

5

7 0 0 8 0 0

Page 4: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

H2 + O2 branching cycle

H + O2

OH+O

H2

H2

H2O + H

H+OH

H2

H2O + H

Overall: H + 3H2 + O2 3H + 2H2O

rb = 2 kb [H][O2]

rds

Page 5: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Mechanism at 2nd limit

balance between chain branching and gas-phase (termolecular) termination

H + O2 3 H rb = 2kb[H][O2]

H + O2 + M HO2 + M rt = kt[H][O2][M]

Page 6: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Then:

where

is the net branching factor.

< 0: evolve to low steady state

> 0: exponential growth

]O][H[]H[

2 itbi rrrrdt

d

]M[2 tb kk

Page 7: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Condition for limit

Critical condition is = 0

2 kb = kt [M]

crRTEE

t

b peA

ART tb /)(2

T

p = 0

< 0

> 0s lo w re ac tio n

ig n itio n

Page 8: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Studies in flow reactors

• Continuous-flow, well-stirred reactor (CSTR)

• Also shows p-Ta ignition limits

• Study in vicinity of 2nd limit

Page 9: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

p-Ta diagram for H2 + O2 in CSTR

0

1 0

2 0

3 0

4 0

5 0

p/to

rr

am b ien t tem p e ra tu re T /Ka

6 5 0 7 0 0 7 5 0 8 0 0

s lo w re ac tio ns tea d y ig n iteds ta te

o sc illa to ryig n itio n

tres = 8 s

Page 10: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Oscillatory ignition

Page 11: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds
Page 12: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

How does oscillation vary with experimental operating conditions?

Page 13: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

“Limit cycles”

Oscillation in time corresponds to “lapping” on limit cycle

Page 14: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Extinction at low Ta

tres = 2 s

Page 15: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

“SNIPER” bifurcation

Page 16: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

More complex behaviour

different oscillations at same operating conditions: birhythmicity

Page 17: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds
Page 18: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Mixed-mode oscillations

H2-rich systems

Page 19: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds
Page 20: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Why do oscillations occur?• Need to consider “third body efficiencies”

remember ignition limit condition

2 kb = kt [M]this assumes all species have same ability to

stabilise HO2-speciesin fact, different species have different

efficiencies: aO2 ~ 0.3, aH2O ~ 6

so: overall efficiency of reacting mixture changes with composition

Page 21: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Allow for this in following way:

In ignition region: > 0, based on reactant composition.

After “ignition”, composition now has H2 and O2 replaced by H2O, so overall efficiency is increased, such that for this composition f < 0.

H2O outflow and H2+O2 inflow causes to increase again – next ignition can develop.

)/(

]OH[]O[]H[2

OHOHOOHH

2OH

2O

2H

22222

2

222

RTpxaxaxk

kkkk

tott

tttb

Page 22: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Explains:

oscillatory nature and importance of flow;

period varies with Ta – through kb;

upper Ta limit to oscillatory region ( > 0 even for “ignited composition”;

extinction of oscillations at ignition limit.

Doesn’t explain:

complex oscillations.

Need to include: a few more reactions + temperature effects

Page 23: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

CO + O2 in closed vessels

• shows p-Ta ignition limit

• chemiluminescent reaction (CO2*) “glow”

• can get “steady glow” and “oscillatory glow” – the lighthouse effect (Ashmore & Norrish, Linnett)

• very sensitive to trace quantities of H-containing species

Page 24: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

CO + O2 in a CSTR• p-T ignition limit diagram shows region of

“oscillatory ignition”

Page 25: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Complex oscillations

Page 26: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Record data under steady operation

Page 27: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Next-maximum map

examplechaotic trace

next-maximumMap

Page 28: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Extent of chaotic region for system with p = 19 mmHg.

parameter lower boundary upper boundary value used

Temperaturea (K) 786 ( 2) 791 ( 2) 789

O2 flowb (sccm) 4.0 ( 0.1) 9.0 ( 0.15) 5.6

CO flowc (sccm) 6.9 ( 0.5) 7.4 ( 0.2) 7.14

sccm = standard cubic centimetre per minute; awith = 5.6 sccm and fCO = 7.14 sccm; bwith T = 789 K and fCO = 7.14 sccm; cwith T = 789 K and = 5.6 sccm.

fO2

fO2

Page 29: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

A quick guide to maps

0.0 0.2 0.4 0.6 0.8 1.00.0

0.2

0.4

0.6

0.8

1.0

Xn+1

Xn

xn+1 = A xn (1 – xn) 1 < A < 4

Page 30: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

A = 2 A = 2.5 A = 3.2

0 0.1 0.1 0.1

1 0.18 0.23 0.29

2 0.30 0.44 0.66

3 0.42 0.61 0.72

4 0.49 0.59 0.64

5 0.5 0.6 0.74

lots 0.5 0.6 0.51

lots + 1 0.5 0.6 0.80

Page 31: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

iteration of the map

Page 32: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Perturbing the map

fixed point shifts

Page 33: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

targeting the fixed point

need to determine : location of fixed point of unperturbed systemslope of map in vicinity of fixed pointshift in fixed point as system is perturbed

Ott, Grebogi, Yorke 1990; Petrov, Peng, Showalter 1991

Page 34: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

experimental strategy

From the experimental time series:

• collect enough data to plot the map

• fit the data to get the fixed point and the slope in its region

• perturb one of the experimental parameters

• determine the new map – fit to find shift in fixed point

Page 35: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

control constant

Can calculate a “control constant” g

where m is the slope of the map and dxF/df is the rate of change of the fixed point with some experimental parameter

df

dx

m

mg F)1(

Note: m and dxF/df can be measured experimentally

Page 36: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Calculate appropriate perturbation

g

xx

dfdxm

mf

F

/1

If we observe system and it comes “near to” the fixed point of the map : x = x xF

Can calculate the appropriate perturbation to the operating conditions

Page 37: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Exploiting the map Chaos control

Map varies with the exptl conditions

Page 38: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Control of Chaosby suitable,very smallamplitudedynamicperturbationscan controlchaos

perturbationsdetermined from Experiment

Davies et al., J. Phys. Chem. A: 16/11/00

Page 39: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

0

2

4

6

8

10

12

0 200 400 600

time, t /s

Flo

w / s

cc

m

Chaotic region

(C)

0.0

2.0

4.0

6.0

8.0

0 200 400 600

time, t /s

Pe

ak

PM

T s

ign

al / m

VControl off

CTT

(B)

Page 40: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

some unexpected features

0.0

1.0

2.0

3.0

4.0

5.0

6.0

0 100 200 300 400 500 600

time, t /s

Pe

ak

PM

T s

ign

al / m

V

Control off

CTT

0.0

1.0

2.0

3.0

4.0

5.0

6.0

7.0

0 100 200 300 400 500 600

time, t /s

Pe

ak

PM

T s

ign

al / m

V

Control offCTT

0.0

1.0

2.0

3.0

4.0

5.0

6.0

7.0

0 100 200 300 400 500 600

time, t /s

Pe

ak

PM

T s

ign

al /

mV

CTT Control off

0.0

1.0

2.0

3.0

4.0

5.0

6.0

0 100 200 300 400 500 600

time, t /s

Pe

ak

PM

T s

ign

al /

mV

Control offCTT

control transient time depends on how long perturbation is applied for

Page 41: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

optimal control occursfor perturbation applied foronly 25% of oscillatory period

Page 42: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Conclusions• Oscillations, including complex oscillations and

even chaotic evolution, arise naturally in chemical reactions as a consequence of “normal” mechanisms with “feedback”

• Chaos occurs for a range of experimental conditions.

• Chaotic systems can be “controlled” using simple experimental strategies

• These need no information regarding the chemical mechanisms and we can determine all the parameters necessary from experiments even if only one signal can be measured

Page 43: Chaos and Control in Combustion Steve Scott School of Chemistry University of Leeds

Acknowledgements

Barry Johnson

Matt Davies, Mark Tinsley, Peter Halford-Maw

Istvan Kiss, Vilmos Gaspar (Debrecen)

British Council – Hungarian Academy

ESF Scientific Programme REACTOR