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Chemical Reactors Fundamentals, Exercises of Chemical Kinetics

Miscellaneous textbook solutions to problems in the Elements of Chemical Reaction Engineering textbook by Fogler

Typology: Exercises

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CBE 450 Chemical Reactor Fundamentals
Fall, 2009
Homework Assignment #1
1. Review of Mass Balances of Reacting Systems
Natural gas (assume pure methane) is being burned in air (assume 0.79 mol% N2 and 0.21 mol%
O2). Assume complete combustion, which means that all of the natural gas is burned and is
converted into carbon dioxide and water. Assume that the oxygen is provided in 100% excess.
The flow rate of natural gas is 100 mol/s. The furnace operates at steady state.
(a) Draw a diagram with all input and output streams. Indicate known and unknown flowrates.
Indicate known and unknown compositions.
(b) Determine the flowrate of air.
(c) Determine the flowrate and composition of the output gas using atomic balances.
(d) Determine the flowrate and composition of the output gas using molecular balances.
Solution
(a) Draw a diagram with all input and output streams. Indicate known and unknown flowrates.
Indicate known and unknown compositions.
(b) Determine the flowrate of air.
The balanced reaction is
CH4 + 2O2 CO2 + 2H2O
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CBE 450 Chemical Reactor Fundamentals Fall, 2009 Homework Assignment #

1. Review of Mass Balances of Reacting Systems

Natural gas (assume pure methane) is being burned in air (assume 0.79 mol% N 2 and 0.21 mol%

O 2 ). Assume complete combustion, which means that all of the natural gas is burned and is

converted into carbon dioxide and water. Assume that the oxygen is provided in 100% excess.

The flow rate of natural gas is 100 mol/s. The furnace operates at steady state.

(a) Draw a diagram with all input and output streams. Indicate known and unknown flowrates.

Indicate known and unknown compositions.

(b) Determine the flowrate of air.

(c) Determine the flowrate and composition of the output gas using atomic balances.

(d) Determine the flowrate and composition of the output gas using molecular balances.

Solution

(a) Draw a diagram with all input and output streams. Indicate known and unknown flowrates.

Indicate known and unknown compositions.

(b) Determine the flowrate of air.

The balanced reaction is

CH 4 + 2O 2  CO 2 + 2H 2 O

The stoichiometrically required amount of O 2 is two moles of O 2 for every mole of CH 4. Since

the oxygen is provided in 100% excess, you actually need twice as much, or four moles of O 2 for

every mole of CH 4. Since you have 100 mol/s of CH 4 , you need 400 mol/s of O 2. To determine

the total air flowrate,

AxO 2  A  0. 21   400 mol / s

A mol / s 1905 mol / s

  1. 21

(c) Determine the flowrate and composition of the output gas using atomic balances.

We have five unknowns, the flowrate and four compositions of the stack gas. Therefore, we

need five equations. The first four equations are atom balances of the form:

accumulation = in – out + generation

The accumulation term is zero because the furnace is operating at steady state. The generation

term is zero because atoms are neither created or destroyed in this furnace. Therefore, the atom

balance is

in = out

N: 2 AxN (^) 2  2 SzN 2

C: FyCH (^) 4  SzCO 2

H: 4 Fy (^) CH (^) 4  2 SzH 2 O

O: 2 AxO (^) 2  2 SzO 2  2 SzCO 2  SzH 2 O

The fifth equation is the sum of the mole fractions is unity

sum of the mole fractions is unity: 1  zO (^) 2  zCO 2  zH 2 OzN 2

Now solve.

in = out

N: SzN 2  AxN 2  1505

C: SzCO 2  FyCH 4  100

N 2 : 0  AxN (^) 2  SzN 2

CO 2 : 0  0  SzCO 2 ( 1 ) 100

H 2 O: 0  0  SzH 2 O ( 2 ) 100

O 2 : 0  AxO 2  SzO 2 ( 2 ) 100

CH 4 : 0  FyCH 4  0 ( 1 ) 100

We see that the methane balance was actually used to determine the generation term.

The fifth equation is the sum of the mole fractions is unity

sum of the mole fractions is unity: 2 2 2 2

1  zOzCOzHOzN

Now solve.

N 2 : SzN 2  AxN 2  1505

CO 2 : SzCO 2  100

H 2 O: SzH 2 O  200

O 2 : SzO 2  AxO 2  200  200

We can multiply the mole fractions sum by S and write

SSzO 2  SzCO 2  SzH 2 OSzN 2  200  100  200  1505  2005 mol / s

The compositions are thus

N:

2 ^  

S

z (^) N

C:

2 ^  

S

z (^) CO

H:

2 ^  

S

z (^) HO

O:

2 ^  

S

z (^) O

This is the same result as was obtained from the atomic balances, as it must be.

2. Molecular Description of Reaction Equilibrium

Consider the distribution of para-xylene, meta-xylene and ortho-xylene.

(a) For an ideal gas at a given temperature, what factors at the molecular level determine the

equilibrium distribution of components?

(b) At a given temperature, will the mole faction of the component with the lowest enthalpy be

greater or less than the mole fraction of the other components (all other things being equal)?

Why?

(c) At a given temperature, will the mole faction of the component with the lowest entropy be

greater or less than the mole fraction of the other components (all other things being equal)?

Why?

(d) At a given temperature, will the mole faction of the component with the lowest free energy be

greater or less than the mole fraction of the other components (all other things being equal)?

Why?

(e) As the temperature is increased, will the mole fraction of the component with the lowest

enthalpy increase or decrease (all other things being equal)? Why?

(f) As the temperature is increased, will the mole fraction of the component with the lowest

entropy increase or decrease (all other things being equal)? Why?

Solution:

(a) For an ideal gas at a given temperature, what factors at the molecular level determine the

equilibrium distribution of components?

At the molecular level, the enthalpy and the entropy can be broken into contributions from

translation of the center of the mass of the molecule rotation about the center of mass of the molecule vibration of bonds within the molecule internal rotation of internal rotors like the methyl groups in xylene

The total enthalpy and entropy (and thus the free energy) are related to these contribution. Thus

the equilibrium distribution is based on these contributions.

(b) At a given temperature, will the mole faction of the component with the lowest enthalpy be

greater or less than the mole fraction of the other components (all other things being equal)?

Why?

RT

H

R

S

RT

H T S

RT

G

K

N

N

eq

12 12 12 12 12 , 12 2

(^1) exp exp exp exp

A low free energy state is favored at equilibrium.

(e) As the temperature is increased, will the mole fraction of the component with the lowest

enthalpy increase or decrease (all other things being equal)? Why?

If state one has the lowest enthalpy, then  H (^) 1  2  0 and  S 1 (^)  2  0 , then the derivative of this

distribution with respect to temperature is

exp exp 2 0 12 12 12

2

1  

RT

H

RT

H

R

S

N

N

T

where we neglected the temperature dependence of the enthalpies of formation. So as the

temperature increases the relative amount of N 1 decreases. In other words, the low energy state

is more favored at low temperature.

(f) As the temperature is increased, will the mole fraction of the component with the lowest

entropy increase or decrease (all other things being equal)? Why?

If state one has the lowest entropy, then  S 1 (^)  2  0 and  H 1 (^)  2  0 , then the derivative of this

distribution with respect to temperature is

exp exp 2 0 12 12 12

2

1  

RT

H

RT

H

R

S

N

N

T

where we neglected the temperature dependence of the enthalpies of formation. So as the

temperature increases the relative amount of N 1 remains unchanged. In other words, the entropic

contribution to the distribution of components does not have a temperature dependence.

3. Review Continuum Description of Reaction Equilibrium

Consider a batch reactor initially containing nitrogen and hydrogen gases. The volume of the

batch reactor is 1 m 3

. The initial pressure is 1 atm. The temperature is kept constant at 500 K.

The initial mole fractions are 0.25 N 2 and 0.75 H 2. The relevant reaction is

N 2  3 H 2  2 NH 3

The reference enthalpies of formation are at a reference temperature of 298.15 K

H (^) f , N 2  0 kcal / mol

H (^) f , H 2  0 kcal / mol

H (^) f , NH 3  10. 96 kcal / mol

The reference Gibbs free energies of formation are at a reference temperature of 298.15 K

G (^) f , N 2  0 kcal / mol

G (^) f , H 2  0 kcal / mol

G (^) f , NH 3  3. 903 kcal / mol

In this project, you may assume that the heat capacities are constant, given by

C (^) p , N 2  7. 03 cal / mol / K

C (^) p , H 2  6. 92 cal / mol / K

C (^) p , NH 3  9. 31 cal / mol / K

(a) What are the heats of formation at 500 K for each component?

   ^ ^ 

T

T

fi fi ref pi ref

H (^) , T H , T C , dT

For constant heat capacities

H f , i  T   Hf , i  T ref   Cp , i  T  Tref 

H f N  T K   500 298  1. 42 kcal / mol

, (^2)

H f H  T K   500 298  1. 40 kcal / mol

, 2 ^500 ^0.^0   

H f N  T K   500 298  9. 08 kcal / mol

, (^2)

(b) What are the free energies of formation at 500 K for each component. (You may assume that

the heat of formation is constant in this part (b) calculation only.)

T

T

fi fi ref ref

fi ref

dT T

H

G T T

T

T

G T 2

, , ,

For constant heats of formation,

ref

fi ref fi ref

f i T T

G T TH

T

T

G T

, , ,

   24. 4 i

N No i

The number of each species is

N j  No , j   j 

NN 2  No , N 2   N 2  6. 09  0. 5 

NH 2  No , H 2  H 2  18. 3  1. 5 

NNH 3  No , NH 3  NH 3  0. 0  1. 0 

The reference pressure is 101325 Pa.

The final pressure is (using the ideal gas law)

V

N RT

V

NRT

p

i

o  i ^ 

Substituting these into equations the equilibrium coefficient  

1 / 2 2

3 / 2 2

3 1 / 2 2

3 / 2 2

3

1

H N

NH

H N

NH

ref

eq x x

x

x x

x

p

p K  

   

3 / 2 1 / 2

1

3 / 2 1 / 2

1

 

 

 

ref ref

eq p

p

p

p K

Solving this single, non-linear algebraic equation, I find

and mole fractions

N

N

x

oj j j

,^ ^ 

xN

xH

xNH