Coupled Chemical and Thermal Analysis
Transcript of Coupled Chemical and Thermal Analysis
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Well-Stirred Reactor -1
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Coupled Chemical and Thermal
Analysis: Well-Stirred ReactorJerry Seitzman
Methane Flame
0
0.05
0.1
0.15
0.2
0 0.1 0.2 0.3
Distance (cm)
M o l e F r a c t i o n
0
500
1000
1500
2000
2500
T e m p e r a t u r e ( K )
CH4
H2O
HCO x 1000
Temperature
Well-Stirred Reactor -2
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
• Examine flow reactor where Damix= mix / chem<< 1 – high rate of mixing/stirring
– well-stirred reactor
(WSR )
perfectly-stirred reactor
(PSR )
continuously-stirred reactor (CSR )• Useful for examining
– highly mixed IC engines
– low p, low speed reactors (fast molec. diffusion)
– highly turbulent parts of nonpremixed combustors
– residence time issues and high T chemical kinetics
Well-Stirred Reactor
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Well-Stirred Reactor -3
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Longwell Reactor (circa 1950)
• Fuel injected from holes in central spinning sphere
ref: Turns
Inlet
Outlets
Well-Stirred Reactor -4
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Multiple Reactors
• Simplified swirling pulverized coal combustorflame into network of well-stirred and plug flowreactors
ref: Kee, Coltrin and Glarborg
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Well-Stirred Reactor -5
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
• Normally specify inlet conditions
• Interior properties
Conditions
ini
in
in
Y
T
m
,
ou t i
ou t
ou t
Y
T
m
,
iY T ,
Q
– fast mixing means
internal T , Y i
same as outlet
• Results will depend on residence time
• Can develop for various heat transfer conditions – known reactor T
– adiabatic – Q fixed or Q(t )
• Can also examine steady or unsteady inlet conditions
Well-Stirred Reactor -6
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
• Species
Governing Equations
• Mass
ini
in
in
Y
T
m
,
ou t i
ou t
ou t
Y
T
m
,
iY T ,
Q
CS
i
CV
i
CM
i
CV
ii Ad nuY dV Y dt d
dt dmdV W ˆ
iniiniout out ini
i Y mY mmmY dt
dY V
,
Reynolds Transport Theorem
iniiniout
i
ii Y mY m
dt
VY d V W
,
CS CV
Ad nudV dt
d ˆ0
out in
mmdt
V d
(III.11)
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Well-Stirred Reactor -7
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Governing Equations
• Species (con’t)
iniiniout out ini
i
ii Y mY mmmY
dt
dY V V W
,
ii
iini
ini W
Y Y V
m
dt
dY
,
iniiin
i
ii Y Y mdt
dY V V W
,
res
inin m
m
m
V
• Residence Time
(III.12)
(III.13)
Well-Stirred Reactor -8
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Governing Equations
• Energy
CS CV
inin Ad nuhedV
dt
d QW ˆ
iniinin Y T m
,
,,
ou t i
ou t
ou t
Y
T
m
,
iY T ,
Q
dt
dpV hhm
dt
dhV Q
ininin
dt
dphh
V
m
V
Q
dt
dhin
inin
1
ininin hmhm
dt
hV d Q
dt
dV p
p
inininin
hmhmdt dV p
dt pV d mmh
dt dhV Q
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Well-Stirred Reactor -9
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Governing Equations
• Energy (con’t)
– use state eqn’s. for hT
i
i
imix pdt
dY h
dt
dT c
dt
dh
i
iiiniiniin hY hY hh
,,
dt
dpqW h
hhY V
m
dt
dT
c ini
iii
iiiniini
in
mix p
1,,
i
ii
iini
in
i
W Y Y
V
mh
,
chemq
res 1
(III.14)
dt
dphh
V
m
V
Q
dt
dhin
inin
1
Well-Stirred Reactor -10
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Summary: Governing Equations
• Mass
• Species
• Energy
• Variables
– inputs
– unknowns
dt dp
qW h
hhY V
m
dt
dT c in
N
iiii
iiiniini
in
mix p
1
,,
ou t in
mmdt
V d
ii
iini
ini W
Y Y V
m
dt
dY
,
inininiin qT Y m ,,,
,
pT Y N mV iout
,,,,, T R p
mix
– 2+ N ODE’s, 1 algebraic need 2 more constraintse.g., V (t ) and p(t )
(III.11)
(III.12)
(III.14)
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Well-Stirred Reactor -11
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Steady-State Solutions
• Mass
• Species
• Energy
• Variables
– inputs
– unknowns
in
N
iiii
iiiniini
in q
W hhhY
V
m
1
,,0
mmmout in 0
ii
iini
W Y Y
V
m
,0
pV qT Y mininini
,,,,,,
T Y N i ,, T R p
mix
– 2+ N coupled nonlinear algebraic eqs. solvable
Well-Stirred Reactor -12
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Steady WSR Analytic Soln
• Species
• Energy
iniiii
resi
iniiini
qW h
hhY
,,
ii
resinii
W Y Y
,
in pi
iniiini T T chhY ,,
P O F
RT E
F
F
F
aeW
Y B
A[Ox ] [F ]
• Simplify
– assume c p constant andsame for all species
– single-step reaction
– Arrhenius rate expression
lean mixture, oxidizer
concentration ~constant
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Well-Stirred Reactor -13
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Energy: Steady WSR
• Energy
in
loss
P P OO F F
RT
E
F
F
resin pinOin F m
QW hW hW h Be
W
Y T T cY Y
a
,,
in
loss
P f O f F f
RT E
F
res F
in pm
Qhhh Be
W
Y T T c a
,,,
in
loss RT E
res F in p
m
Q HV BeY T T c a
in
N
iiii
iiiniini
in q
W hhhY
V
m
1
,,0
pin
loss RT E
p
res F
incm
Q HV e
c
BY T T a
heating
value
Well-Stirred Reactor -14
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Normalized Adiabatic Equations
• Species
• Energy
RT E
F resin F F
ae BY Y Y ,
HV ec
BY T T
RT E
p
F res
in
a
T E aea DY Y 1
T E aea DY V H T 1
resinin F F Ba DT T T Y Y Y ;;
,
in pin F inaa T c HVY V H RT E E ,;
T E aea DV H T T 110
• Normalizations
– norm. eq’s.
– combineT E
T E
a
a
ea D
ea DV H
1
1
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Well-Stirred Reactor -15
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Solution Limits: Da
• Examine solution limits with Damköhler number
– Da0
slow chemistry
– Da
fast chemistry
T E aea DV H T T 110
)1and(1 Y T
)0and(1 Y V H T
• What happens in between? – examine solutions for various E a
inin F F T T T Y Y Y ;
,
Well-Stirred Reactor -16
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Residence Time Effects
1.0
1.5
2.0
2.5
3.0
3.5
4.0
4.5
5.0
0.01 0.1 1 10 100 1000
Da'
T '
Ea'=2 5 10
Q
HV =4
I
res
inin m
m
m
V
res Ba D
inT T T
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Well-Stirred Reactor -17
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
1.0
1.5
2.0
2.5
3.0
3.5
4.0
4.5
5.0
0.01 0.1 1 10 100 1000 10000 100000
Da'
T '
Ea'=2 5 10 15
Residence Time Effects
HV =4
res Ba D
inT T T
Well-Stirred Reactor -18
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Ignition/Extinction
• For low activation energies ( E a /T )
– no distinct ignition/extinction phenomena
– small changes in T do not change reaction rates
• For high activation energy ( E a /T )
– multivalued solutions
– upper (>Q) and lower (< I ) branches stable
– middle branch unstable (hysteresis);
leads to extinction and ignition temperatures/
residence times
– for large E a/T , Ignition/Extinction separate more
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Well-Stirred Reactor -19
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Blowout Limits
• Can use this approach to model minimum residence
times (maximum mass flow rates) to prevent
blowout in gas turbine combustors
Stable1
nVpm
0.4
Blowout
Well-Stirred Reactor -20
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Transient Reactor: Oscillating Ignition
• Sinusoidal forcing
of reactor volume
close to ignition
conditions
• Low frequencies
shorter delays
%4V V rms
H2/“Air”; =1; 1atm
ref: Kee, Coltrin and Glarborg
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Well-Stirred Reactor -21
School of Aerospace Engineering
Copyright © 2004-2005 by Jerry M. Seitzman. All rights reserved.AE/ME 6766 Combustion
Transient Reactor: Oscillating Ignition
• Net radical production increase during each cycle
– nonlinear T dependence produces more radicals
during compression than lost during expansion
ref: Kee, Coltrin and GlarborgH2/“Air”; =1; 1atm
2500 Hz