Coupled Chemical and Thermal Analysis

11
7/27/2019 Coupled Chemical and Thermal Analysis http://slidepdf.com/reader/full/coupled-chemical-and-thermal-analysis 1/11 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 Reactor Jerry 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 Da mix = 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  chemical kinetics Well-Stirred Reactor

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

m

,

ou t i

ou t 

ou 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

m

,

ou t i

ou t 

ou 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 

m

,

iY T ,

Q

dt 

dpV hhm

dt 

dhV Q

ininin      

dt 

dphh

m

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 

mh

  

 

  

,

chemq 

res 1

(III.14)

dt 

dphh

m

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 

m  

 

 

1

,,0

mmmout in    0

  

 

  ii

iini

W Y Y 

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

Y T T cY Y 

a

 ,,

  in

loss

 P  f  O f   F  f  

 RT  E 

 F 

res F 

in pm

Qhhh Be

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 

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