Fundamentals Of Chemical Engineering Thermodynamics
Fundamentals Of Chemical Engineering Thermodynamics
1st Edition
ISBN: 9781111580711
Author: Kevin D. Dahm, Donald P. Visco, Jr.
Publisher: CENGAGE L
Question
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Chapter 5.7, Problem 13P

(A)

Interpretation Introduction

Interpretation:

The flow rate of the supercritical methane entering the flash chamber.

Concept Introduction:

The energy balance with an initial mass flow rate of supercritical stream is,

m˙in=m˙liq+m˙vap

Here, initial mass flow rate of supercritical stream is m˙in, mass flow rate of liquid stream is m˙liq, and mass flow rate of vapor stream is m˙vap

The energy balance equation for the system is,

m˙inH^in=m˙liqH^liq+m˙vapH^vap

Here, initial specific enthalpy of supercritical methane is H^in, specific enthalpy of liquid methane is H^liq, and specific enthalpy of vapor methane is H^vap.

(B)

Interpretation Introduction

Interpretation:

The work done for each of the two compressors.

Concept Introduction:

The expression to obtain the reversible work rate of shaft for the eversible compressor 1 with respect to mass flow rate (W˙S,rev,c1/m˙) is,

W˙S,rev,c1/m˙=H^out,rev,c1H^in,c1η

Here, reversible work rate of shaft for the eversible compressor 1 is W˙S,rev,c1, mass flow rate is m˙, and efficiency is η.

The expression to obtain the actual work (W1) for compressor 1 is,

W1=(W˙S,rev,c1/m˙)(m˙in)

The expression to obtain the reversible work rate of shaft for the eversible compressor 2 with respect to mass flow rate (W˙S,rev,c2/m˙) is,

W˙S,rev,c2/m˙=H^out,rev,c2H^in,c2η

Here, reversible work rate of shaft for the eversible compressor 2 is W˙S,rev,c2.

The expression to obtain the actual work (W2) for compressor 2 is,

W2=(W˙S,rev,c2/m˙)(m˙in)

(C)

Interpretation Introduction

Interpretation:

The heat transfer for each of the four heat exchangers.

Concept Introduction:

The expression to obtain the actual initial specific enthalpy of entering methane for compressor 1 (H^in,act,c1) is,

H^in,act,c1=H^in,c1+W˙S,rev,c1/m˙

The expression to obtain the actual final specific enthalpy of entering methane for compressor 2 (H^out,act,c2) is,

H^out,act,c2=H^in,c1+W˙S,rev,c1/m˙

The energy balance equation for HX2 and HX3 is,

Q˙m˙in=H^outH^in

Here, rate of heat added or removed from the system is Q˙, final specific enthalpy is H^out, and an initial specific enthalpy is H^in.

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