General Information on Main Equations of State: Ideal Gas Law Van

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General Information on Main Equations of State:
1. Ideal Gas Law
๐‘ƒ๐‘‰ = ๐‘›๐‘…๐‘‡
2. Van der Waals
๐‘Ž
(๐‘ƒ + 2 ) (๐‘‰๐‘š − ๐‘) = ๐‘…๐‘‡
๐‘‰๐‘š
๐‘คโ„Ž๐‘’๐‘Ÿ๐‘’ ๐‘‰๐‘š ๐‘–๐‘  ๐‘š๐‘œ๐‘™๐‘Ž๐‘Ÿ ๐‘ฃ๐‘œ๐‘™๐‘ข๐‘š๐‘’ ๐‘Ž๐‘›๐‘‘ ๐‘กโ„Ž๐‘’ ๐‘ ๐‘ข๐‘๐‘ ๐‘ก๐‘Ž๐‘›๐‘๐‘’
− ๐‘ ๐‘๐‘’๐‘๐‘–๐‘“๐‘–๐‘ ๐‘๐‘œ๐‘›๐‘ ๐‘ก๐‘Ž๐‘›๐‘ก๐‘  ๐’‚ ๐‘Ž๐‘›๐‘‘ ๐’ƒ ๐‘๐‘Ž๐‘› ๐‘๐‘’ ๐‘๐‘Ž๐‘™๐‘๐‘ข๐‘™๐‘Ž๐‘ก๐‘’๐‘‘ ๐‘“๐‘Ÿ๐‘œ๐‘š ๐‘กโ„Ž๐‘’ ๐‘๐‘Ÿ๐‘–๐‘ก๐‘–๐‘๐‘Ž๐‘™ ๐‘๐‘Ÿ๐‘œ๐‘๐‘’๐‘Ÿ๐‘ก๐‘–๐‘’๐‘  ๐‘ƒ๐‘ , ๐‘‡๐‘ ๐‘Ž๐‘›๐‘‘ ๐‘‰๐‘
27(๐‘…๐‘‡๐‘ )2
2
๐‘Ž = 3๐‘ƒ๐‘ ๐‘‰๐‘ =
64๐‘ƒ๐‘
๐‘‰๐‘ ๐‘…๐‘‡๐‘
๐‘= =
3
8๐‘ƒ๐‘
3. Redlich-Kwong
- Superior to Van der Waals, but performs poorly with respect to liquid phase and
therefore cannot be used for calculating vapor-liquid equilibria
๐‘…๐‘‡
๐‘Ž
๐‘ƒ=
−
๐‘‰๐‘š − ๐‘ √๐‘‡๐‘‰๐‘š (๐‘‰๐‘š + ๐‘)
0.42748๐‘… 2 ๐‘‡๐‘2.5
๐‘Ž=
๐‘ƒ๐‘
0.08662๐‘…๐‘‡๐‘
๐‘=
๐‘ƒ๐‘
- Good for calculations of gas phase properties when the ratio of the pressure to
the critical pressure is less than about one-half of the ratio of the temperature to
the critical temperature:
๐‘ƒ
๐‘‡
<
๐‘ƒ๐‘ 2๐‘‡๐‘
4. Peng-Robinson
๐‘…๐‘‡
๐‘Ž๐›ผ
๐‘ƒ=
− 2
๐‘‰๐‘š − ๐‘ ๐‘‰๐‘š + 2๐‘๐‘‰๐‘š − ๐‘ 2
0.457235๐‘… 2 ๐‘‡๐‘2
๐‘Ž=
๐‘ƒ๐‘
0.077796๐‘…๐‘‡๐‘
๐‘=
๐‘ƒ๐‘
2
๐›ผ = (1 + ๐œ…(1 − ๐‘‡๐‘Ÿ0.5 ))
๐œ… = 0.37464 + 1.54226๐œ” − 0.26992๐œ”2
๐‘‡
๐‘‡๐‘Ÿ =
๐‘‡๐‘
Question 3
Small hydrocarbons are often liquefied for ease of transport. Consider the liquefaction of
methane by the Linde process as shown in the diagram below. Methane is fed at 4 bar and
295 K where it is mixed with uncondensed vapor at 4 bar and 290 K. The stream is then fed
to a compressor where it is compressed to 60 bar and then cooled isobarically (ΔP=0) to
295 K. This stream then exchanges heat with the vapor stream leaving the throttle (no
mass between the streams is exchanged; process is adiabatic). The vapor stream leaving
the heat exchanger is then throttled isenthalpically (ΔH=0) and adiabatically (ΔQ=0) to
4 bar, dropping the temperature of the vapor and liquid streams leaving the throttle in
equilibrium sufficient to liquefy some of the methane. The uncondensed methane vapor
exchanges heat with the incoming stream and then is mixed with the feed. Using a
volumetric flow rate of 100 L/s leaving the compressor as a basis of calculation, answer the
following questions:
a. (10 pts) Solve for the molar flow rate of the methane leaving the compressor.
Explicitly state what equation of state you are using and why.
Given: P = 6bar = 5.921atm , T = 295K, R=0.082L*atm/K*mol
Use ideal gas law
๐‘ท๐‘ฝฬ‡ = ๐’ฬ‡ ๐‘น๐‘ป
๐‘ท๐‘ฝฬ‡
(๐Ÿ“. ๐Ÿ—๐Ÿ๐Ÿ๐’‚๐’•๐’Ž)(๐Ÿ๐ŸŽ๐ŸŽ ๐‘ณ⁄๐’”)
๐’ฬ‡ =
=
= ๐Ÿ๐Ÿ’. ๐Ÿ’๐Ÿ– ๐’Ž๐’๐’⁄๐’”
๐‘น๐‘ป (๐ŸŽ. ๐ŸŽ๐Ÿ–๐Ÿ ๐‘ณ๐’‚๐’•๐’Ž⁄๐‘ฒ๐’Ž๐’๐’)(๐Ÿ๐Ÿ—๐Ÿ“๐‘ฒ)
b. (10 pts) What is the temperature (in K) of the liquid methane leaving the
throttler? Hint: this liquid stream and the leaving vapor stream share the
same temperature and pressure.
Heat Exchanger is isenthalpic and adiabatic
Use the following equation to solve for outlet temp of heat exchanger
๐’…๐‘ฏ = ๐ŸŽ = ๐‘ช๐’‘ ๐’…๐‘ป
๐‘ช๐‘ท ๐’‡๐’๐’“ ๐’Ž๐’†๐’•๐’‰๐’‚๐’๐’† ๐’ˆ๐’‚๐’” = ๐ŸŽ. ๐ŸŽ๐Ÿ๐Ÿ—๐Ÿ–๐Ÿ• + ๐Ÿ“. ๐ŸŽ๐Ÿ๐Ÿ ∗ ๐Ÿ๐ŸŽ−๐Ÿ“ ๐‘ป
๐‘ป๐’‡
๐ŸŽ = ∫ (๐ŸŽ. ๐ŸŽ๐Ÿ๐Ÿ—๐Ÿ–๐Ÿ• + ๐Ÿ“. ๐ŸŽ๐Ÿ๐Ÿ ∗ ๐Ÿ๐ŸŽ−๐Ÿ“ ๐‘ป)๐’…๐‘ป
๐Ÿ๐Ÿ—๐Ÿ“
= (๐ŸŽ. ๐ŸŽ๐Ÿ๐Ÿ—๐Ÿ–๐Ÿ•๐‘ป๐’‡ + ๐Ÿ. ๐ŸŽ๐ŸŽ๐Ÿ’ ∗ ๐Ÿ๐ŸŽ−๐Ÿ’ ๐‘ป๐Ÿ๐’‡ )
− (๐ŸŽ. ๐ŸŽ๐Ÿ๐Ÿ—๐Ÿ–๐Ÿ•๐‘ป๐Ÿ๐Ÿ—๐Ÿ“ + ๐Ÿ. ๐ŸŽ๐ŸŽ๐Ÿ’ ∗ ๐Ÿ๐ŸŽ−๐Ÿ’ ๐‘ป๐Ÿ๐Ÿ๐Ÿ—๐Ÿ“ )
๐ŸŽ = ๐Ÿ. ๐ŸŽ๐ŸŽ๐Ÿ’ ∗ ๐Ÿ๐ŸŽ−๐Ÿ’ ๐‘ป๐Ÿ๐’‡ + ๐ŸŽ. ๐ŸŽ๐Ÿ๐Ÿ—๐Ÿ–๐Ÿ•๐‘ป๐’‡ − ๐Ÿ“. ๐Ÿ–๐Ÿ—๐Ÿ
Use quadratic equation to solve for Tf
−๐ŸŽ. ๐ŸŽ๐Ÿ๐Ÿ—๐Ÿ–๐Ÿ• ± √๐ŸŽ. ๐ŸŽ๐ŸŽ๐ŸŽ๐Ÿ‘๐Ÿ—๐Ÿ’๐Ÿ– − ๐Ÿ’ ∗ ๐ŸŽ. ๐ŸŽ๐ŸŽ๐ŸŽ๐Ÿ๐ŸŽ๐ŸŽ๐Ÿ’ ∗ −๐Ÿ“. ๐Ÿ–๐Ÿ—๐Ÿ
๐‘ป๐’‡ =
๐Ÿ ∗ ๐ŸŽ. ๐ŸŽ๐ŸŽ๐ŸŽ๐Ÿ๐ŸŽ๐ŸŽ๐Ÿ’
−๐ŸŽ. ๐ŸŽ๐Ÿ๐Ÿ—๐Ÿ–๐Ÿ• ± ๐ŸŽ. ๐ŸŽ๐Ÿ“๐Ÿ๐Ÿ“
๐‘ป๐’‡ =
= ๐Ÿ๐Ÿ”๐Ÿ‘. ๐Ÿ๐Ÿ“๐‘ฒ
๐ŸŽ. ๐ŸŽ๐ŸŽ๐ŸŽ๐Ÿ
Throttle is adiabatic
๐‘ธ = ๐ŸŽ = ๐’Ž๐’„๐šซ๐‘ป
No change in temperature because both m & c are held constant
๐‘ป๐’๐’–๐’• = ๐Ÿ๐Ÿ”๐Ÿ‘. ๐Ÿ๐Ÿ“๐‘ฒ
c. (20 pts) Use an energy balance to find the moles of liquid methane that leave
the throttler. Approximate heat capacity date is listed. You can neglect
isothermal pressure changes for the liquid, but since the methane vapor is
not ideal you will have to calculate the enthalpy change for isothermal
pressure changes using the following empirical relation:
๐‘˜๐ฝ
๐‘๐‘Ž๐‘Ÿ โˆ™ ๐‘š๐‘œ๐‘™
The hat above the H means it’s the partial enthalpy of methane
ฬ‚ = ๐‘Ž [๐‘ƒ2 − ๐‘ƒ1 ]; ๐‘Ž = −0.018
๐ป
๐‘ธ = ๐ŸŽ = ๐šซ๐‘ฏ = ∑ ๐’๐’Š ๐‘ฏ๐’Š − ∑ ๐’๐’Š ๐‘ฏ๐’Š
๐’๐’–๐’•
๐’Š๐’
= ๐’๐’๐’–๐’•,๐’— ๐‘ฏ๐’๐’–๐’•,๐’ + ๐’๐’๐’–๐’•,๐’ ๐‘ฏ๐’๐’–๐’•,๐’ − ๐’๐’Š๐’,๐’— ๐‘ฏ๐’Š๐’,๐’— − ๐’๐’๐’–๐’•,๐’ ๐‘ฏ๐’๐’–๐’•,๐’
ฬ‚
๐ŸŽ = ๐’๐’— ๐‘ฏ๐’— − ๐’๐’ ๐šซ๐‘ฏ๐’
ฬ‚ ๐’— = ๐’‚(๐‘ท๐Ÿ − ๐‘ท๐Ÿ )
๐‘ฏ
Antoine equation constants: Log10(P*)=A – B/(T+C) P* in bar; T in K
Substance
A
B
C
Methane
3.9895 443.028 -0.49
Substance
Methane liquid
Methane vapor
Cp (kJ/mol-K)
.05293
.01987+5.021e-05*T (T in K)
)
Question 5
An air stream at 25oC and 1 atm is contaminated with 4 mol% benzene vapor. To
satisfy EPA and OSHA requirements, 85% by mass of the incoming benzene must be
stripped from the air stream. To accomplish this, the on-site engineer has
constructed a compressor/condenser to pressurize the incoming stream
isothermally (๐šซ๐‘ป = ๐ŸŽ). Two streams emerge from the compressor/condenser in
equilibrium at 25oC: an air stream with the reduced concentration of benzene, and a
stream of pure liquid benzene. Using a basis of 100 L(STP)/s of the incoming air
stream, answer the following questions:
a. (5 pts) What is the molar flow rate of the incoming air stream in mol/s?
Basis = 100L/s for incoming air stream
Ideal gas at STP: 24L/mol
๐Ÿ๐ŸŽ๐ŸŽ๐‘ณ ๐Ÿ๐’Ž๐’๐’
∗
= ๐Ÿ’. ๐Ÿ๐Ÿ”๐Ÿ•๐’Ž๐’๐’/๐’”
๐’”
๐Ÿ๐Ÿ’๐‘ณ
Molar flow rate of air:
๐Ÿ’. ๐Ÿ๐Ÿ”๐Ÿ• ∗ ๐ŸŽ. ๐Ÿ—๐Ÿ” = ๐Ÿ’๐’Ž๐’๐’/๐’”
Sidenote:
MW of benzene (C6H6) = 78.11g/mol
MW of Air (79% N2, 21% O2)=
(0.79*28g/mol)+(0.21*32g/mol)=28.84g/mol
b. (15 pts) What pressure (in atm) are the benzene liquid and benzene/air
stream leaving the compressor? To solve this, first compute the molar
fraction of benzene in the exit air stream.
Molar flow rate of benzene in inlet stream = 0.167mol/s
Mass flow rate of benzene in inlet stream = 0.167*78.11=13.04g/s
Mass flow rate of benzene in outlet stream = 13.04*0.15=1.96g/s
Molar flow rate of benzene in outlet stream = 1.96/78.11=0.025mol/s
For isothermal process we can use the following total balance:
๐‘ท๐’Š๐’ ๐‘ฝ๐’Š๐’ = ๐‘ท๐’๐’–๐’• ๐‘ฝ๐’๐’–๐’• = ๐‘ท๐’ ๐‘ฝ๐’ + ๐‘ท๐’— ๐‘ฝ๐’—
(๐Ÿ๐’‚๐’•๐’Ž)(๐Ÿ๐ŸŽ๐ŸŽ๐‘ณ) = ๐‘ท๐’ ๐‘ฝ๐’ + ๐‘ท๐’— ๐‘ฝ๐’—
We also know the following V & P values:
๐‘ฝ๐’— = ๐‘ฝ๐’—,๐‘ช๐Ÿ” ๐‘ฏ๐Ÿ” + ๐‘ฝ๐’— ๐’‚๐’Š๐’“
๐‘ฝ๐’Š๐’,๐’‚๐’Š๐’“ = ๐‘ฝ๐’—,๐’‚๐’Š๐’“ = (๐Ÿ’๐’Ž๐’๐’)(๐Ÿ๐Ÿ’ ๐‘ณ⁄๐’Ž๐’๐’) = ๐Ÿ—๐Ÿ”๐‘ณ
⇒ ๐‘ฝ๐’—,๐‘ช๐Ÿ” ๐‘ฏ๐Ÿ” = ๐‘ฝ๐’— + ๐Ÿ—๐Ÿ”
๐‘ฝ๐’Š๐’ = ๐Ÿ๐ŸŽ๐ŸŽ๐‘ณ = ๐‘ฝ๐’Š๐’,๐‘ช๐Ÿ” ๐‘ฏ๐Ÿ” + ๐‘ฝ๐’Š๐’,๐’‚๐’Š๐’“
๐‘ฝ๐’Š๐’,๐‘ช๐Ÿ” ๐‘ฏ๐Ÿ” = ๐‘ฝ๐’—,๐‘ช๐Ÿ” ๐‘ฏ๐Ÿ” + ๐‘ฝ๐’
๐Ÿ๐Ÿ’๐‘ณ
๐‘ฝ๐’Š๐’,๐‘ช๐Ÿ” ๐‘ฏ๐Ÿ” = ๐ŸŽ. ๐Ÿ๐Ÿ”๐Ÿ•๐’Ž๐’๐’ (
) = ๐Ÿ’. ๐ŸŽ๐ŸŽ๐Ÿ–๐‘ณ
๐Ÿ๐’Ž๐’๐’
⇒ ๐Ÿ’. ๐ŸŽ๐ŸŽ๐Ÿ– = ๐‘ฝ๐’—,๐‘ช๐Ÿ” ๐‘ฏ๐Ÿ” + ๐‘ฝ๐’
๐‘ฝ๐’—,๐‘ช๐Ÿ” ๐‘ฏ๐Ÿ” = ๐Ÿ’. ๐ŸŽ๐ŸŽ๐Ÿ– − ๐‘ฝ๐’
๐’„๐’๐’Ž๐’ƒ๐’Š๐’๐’† ๐’“๐’†๐’… ๐’†๐’’๐’–๐’‚๐’•๐’Š๐’๐’๐’” ๐’‚๐’๐’… ๐’•๐’๐’•๐’‚๐’ ๐’—๐’๐’๐’–๐’Ž๐’† ๐’†๐’’๐’–๐’‚๐’•๐’Š๐’๐’๐’” ๐’‚๐’๐’…
๐’”๐’๐’๐’—๐’† ๐’‚ ๐’”๐’†๐’• ๐’๐’‡ ๐’•๐’˜๐’ ๐’†๐’’๐’–๐’‚๐’•๐’Š๐’๐’๐’” ๐’˜๐’Š๐’•๐’‰ ๐’•๐’˜๐’ ๐’–๐’๐’Œ๐’๐’๐’˜๐’:
๐Ÿ๐ŸŽ๐ŸŽ = ๐‘ฝ๐’— + ๐‘ฝ๐’
๐Ÿ’. ๐ŸŽ๐ŸŽ๐Ÿ– − ๐‘ฝ๐’ = ๐‘ฝ๐’— + ๐Ÿ—๐Ÿ”
๐‘ฝ๐’— =
Use ideal gas law and volumes above to compute pressures:
c. (20 pts) Estimate the energy requirement (in kW) required to drive the
condenser and cool the gases if the compressor does 2.5 kW of work to the
gases. Assume negligible enthalpy changes for compressing gases. (๐šซ๐‘ฏ =
๐ŸŽ)To help your calculations, please use the inlet-outlet enthalpy table on the
next page and explicitly state your reference state(s) directly on the
table!!
Substance
nin (mol/s)
Hin (kJ/mol)
nout (mol/s)
Air(g)
Benzene(v)
Benzene(l)
r.s._________________________________________________________________________
Hout (kJ/mol)
6. (35 pts) In the Haber process, ammonia can be produced from nitrogen and hydrogen
gas. The unbalanced reaction is as follows and occurs isothermally at 400oC and 1 atm:
๐ป2(๐‘”) + ๐‘2(๐‘”) → ๐‘๐ป3(๐‘ฃ)
In order to allow the reaction to proceed isothermally, 320 kW of heat is transferred from
the reactor. Nitrogen and hydrogen are stoichiometrically balanced, and there is no initial
ammonia. For a basis of a fresh feed rate of 100 mol/s of nitrogen, determine the single
pass conversion of nitrogen by answering the following questions:
d. (5 pts) Write a stoichiometrically balanced reaction for the process.
๐Ÿ‘๐‘ฏ๐Ÿ(๐’ˆ) + ๐‘ต๐Ÿ(๐’ˆ) → ๐Ÿ๐‘ต๐‘ฏ๐Ÿ‘(๐’—)
e. (5 pts) Solve the material balances as completely as possible. You won’t be
able to solve all of them– leave the unknown variables in terms of a single
unknown.
Reactive mechanism so do material balances in terms of atomic
components rather than molecules
Nitrogen Balance: input = output
๐Ÿ๐ŸŽ๐ŸŽ๐’Ž๐’๐’ ๐‘ต๐Ÿ
๐Ÿ๐’Ž๐’๐’ ๐‘ต
๐’ฬ‡ ๐Ÿ (๐’Ž๐’๐’ ๐‘ต๐‘ฏ๐Ÿ‘ )
๐Ÿ ๐’Ž๐’๐’ ๐‘ต
๐’ฬ‡ ๐Ÿ (๐’Ž๐’๐’ ๐‘ต๐Ÿ ) ๐Ÿ ๐’Ž๐’๐’ ๐‘ต
(
)(
)=(
)(
)+(
)(
)
๐’”
๐Ÿ ๐’Ž๐’๐’ ๐‘ต๐Ÿ
๐’”
๐Ÿ ๐’Ž๐’๐’ ๐‘ต๐‘ฏ๐Ÿ‘
๐’”
๐Ÿ ๐’Ž๐’๐’ ๐‘ต๐Ÿ
๐Ÿ๐ŸŽ๐ŸŽ = ๐’ฬ‡ ๐Ÿ,๐‘ต๐‘ฏ๐Ÿ‘ + ๐Ÿ๐’ฬ‡ ๐Ÿ,๐‘ต๐Ÿ
Hydrogen Balance: input = output
๐’ฬ‡ ๐Ÿ,๐‘ฏ๐Ÿ (๐’Ž๐’๐’๐‘ฏ๐Ÿ )
๐Ÿ๐’Ž๐’๐’ ๐‘ฏ
)(
)
๐’”
๐Ÿ ๐’Ž๐’๐’ ๐‘ฏ๐Ÿ
๐’ฬ‡ ๐Ÿ (๐’Ž๐’๐’๐‘ต๐‘ฏ๐Ÿ‘ )
๐Ÿ‘๐’Ž๐’๐’ ๐‘ฏ
๐’ฬ‡ ๐Ÿ (๐’Ž๐’๐’ ๐‘ฏ๐Ÿ )
๐Ÿ๐’Ž๐’๐’ ๐‘ฏ
=(
)(
)+(
)(
)
๐’”
๐Ÿ๐’Ž๐’๐’ ๐‘ต๐‘ฏ๐Ÿ‘
๐’”
๐Ÿ ๐’Ž๐’๐’ ๐‘ฏ๐Ÿ
(
ฬ‡ ๐Ÿ = ๐Ÿ‘๐’ฬ‡ ๐Ÿ,๐‘ต๐‘ฏ๐Ÿ‘ + ๐Ÿ๐’ฬ‡ ๐Ÿ,๐‘ฏ๐Ÿ
๐Ÿ๐’๐Ÿ,๐‘ฏ
๐Ÿ‘๐’ฬ‡ ๐Ÿ,๐‘ฏ๐Ÿ = ๐’ฬ‡ ๐Ÿ,๐‘ต๐Ÿ = ๐Ÿ๐ŸŽ๐ŸŽ
๐Ÿ”๐Ÿ”. ๐Ÿ”๐Ÿ• = ๐Ÿ‘(๐Ÿ๐ŸŽ๐ŸŽ − ๐Ÿ๐’ฬ‡ ๐Ÿ,๐‘ต๐Ÿ ) + ๐Ÿ๐’ฬ‡ ๐Ÿ,๐‘ฏ๐Ÿ
−๐Ÿ“๐Ÿ‘๐Ÿ‘. ๐Ÿ‘ = −๐Ÿ”๐’ฬ‡ ๐Ÿ,๐‘ต๐Ÿ + ๐Ÿ๐’ฬ‡ ๐Ÿ,๐‘ฏ๐Ÿ
Overall Balance: ๐’ฬ‡ ๐Ÿ,๐‘ฏ๐Ÿ + ๐’ฬ‡ ๐Ÿ,๐‘ต๐Ÿ = ๐’ฬ‡ ๐Ÿ,๐‘ต๐‘ฏ๐Ÿ‘ + ๐’ฬ‡ ๐Ÿ,๐‘ต๐Ÿ + ๐’ฬ‡ ๐Ÿ,๐‘ฏ๐Ÿ
๐Ÿ๐’Ž๐’๐’ ๐‘ต๐‘ฏ๐Ÿ‘
๐Ÿ๐ŸŽ๐ŸŽ๐’Ž๐’๐’ ๐‘ต๐Ÿ (
) = ๐Ÿ๐ŸŽ๐ŸŽ๐’Ž๐’๐’ ๐‘ต๐‘ฏ๐Ÿ‘
๐Ÿ๐’Ž๐’๐’ ๐‘ต๐Ÿ
๐Ÿ‘๐Ÿ‘. ๐Ÿ‘ + ๐Ÿ๐ŸŽ๐ŸŽ = ๐Ÿ๐ŸŽ๐ŸŽ + ๐’ฬ‡ ๐Ÿ,๐‘ต๐Ÿ + ๐’ฬ‡ ๐Ÿ,๐‘ฏ๐Ÿ
f. (20 pts) Use an energy balance around the reactor to solve for the remaining
material balances. To help your calculations, please use the inlet-outlet
enthalpy table below and explicitly state your reference state(s) directly
on the table!!
Use reference temperature of 25C for all components
Substance
nin (mol/s)
Hin (kJ/mol)
nout (mol/s)
H2
N2
NH3
r.s._________________________________________________________________________
Hout (kJ/mol)
g. (5 pts) Calculate the single pass conversion of nitrogen.
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