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Reversibility Thermodynamics Professor Lee Carkner Lecture 14

Reversibility

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Reversibility. Thermodynamics Professor Lee Carkner Lecture 14. PAL # 13 Entropy. Work needed to power isentropic compressor Input is saturated vapor at 160 kPa From table A-12, v = 0.12348, h 1 = 241.11, s 1 = Output is superheated vapor, P = 900 kPa, s 2 = s 1 = 0.9419 - PowerPoint PPT Presentation

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Page 1: Reversibility

Reversibility

Thermodynamics

Professor Lee Carkner

Lecture 14

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PAL # 13 Entropy Work needed to power isentropic

compressor Input is saturated vapor at 160 kPa

From table A-12, v = 0.12348, h1 = 241.11, s1 =

Output is superheated vapor, P = 900 kPa, s2= s1 = 0.9419 From table A-13, h2 =

Mass flow rate m’ = V’/v = 0.033 / 0.12348 =

Get work from W = m’h W = (0.27)(277.06-241.11) =

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Ideal Gas Entropy

From the first law and the relationships for work and enthalpy we developed:

We need temperature relations for du, dh, dv and dP

ds = cv dT/T + R dv/v ds = cp dT/T + R dP/P

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Solving for s

We can integrate these equations to get the change in entropy for any ideal gas process

s2-s1 = ∫ cp dT/T + R ln (P2/P1)

Either assume c is constant with T or tabulate

results

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Constant Specific Heats

If we assume c is constant:

s2-s1 = cv,ave ln (T2/T1) + R ln (v2/v1)

s2-s1 = cp,ave ln (T2/T1) + R ln (P2/P1)

since we are using an average

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Variable Specific Heats

so = ∫ cp(T) dT/T (from absolute zero to T)

so2 – so

1 = ∫ cp(T) dT/T (from 1 to 2)

s2 – s1 = so2 – so

1 – Ru ln(P2/P1) Where so

2 and so1 are given in the ideal gas

tables (A17-A26)

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Isentropic Ideal Gas

Approximately true for low friction, low heat processes

cv,ave ln (T2/T1) + R ln (v2/v1) = 0

ln (T2/T1) = -R/cv ln (v2/v1)

ln (T2/T1) = ln (v1/v2)R/cv

(T2/T1) = (v1/v2)k-1

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Isentropic Relations

We can write the relationships in different ways all involving the ratio of specific heats k

(T2/T1) = (P2/P1)(k-1)/k

(P2/P1) = (v1/v2)k

Or more compactly Pvk =constant

Note that: R/cv = k-1

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Isentropic, Variable c

Given that a process is isentropic, we know something about its final state

Pr = exp(so/R) T/Pr = vr

(P2/P1) = (Pr2/Pr1)(v2/v1) = (vr2/vr1)

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Isentropic Work

We can find the work done by reversible steady flow systems in terms of the fluid properties

But we know

-w = vdP + dke + dpe

w = -∫ vdP – ke – pe Note that ke and pe are often zero

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Bernoulli

We can also write out ke and pe as functions of

z and V (velocity)

-w = v(P2-P1) + (V22-V2

1)/2 + g(z2-z1)

Called Bernoulli’s equation

Low density gas produces more work

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Isentropic Efficiencies

The more the process deviates from isentropic, the more effort required to produce the work

The ratio is called the isentropic or adiabatic efficiency

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Turbine

For a turbine we look at the difference between the actual (a) outlet properties and those of a isotropic process that ends at the same pressure (s)

T = wa / ws ≈ (h1 – h2a) / (h1 – h2s)

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Compressor

C = ws / wa ≈ (h2s – h1) / (h2a – h1)

For a pump the liquids are incompressible so:

P = ws / wa ≈ v(P2-P1) / (h2a – h1)

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Nozzles

For a nozzle we compare the actual ke at the exit with the ke of an isentropic process ending at the same pressure

N = V22a / V2

2s ≈ (h1 – h2a) / (h1 – h2s)

Can be up to 95%

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Entropy Balance

The change of entropy for a system during a process is the sum of three things Sin = Sout = Sgen =

We can write as:

Ssys is simply the difference between the initial and final states of the system Can look up each, or is zero for isentropic processes

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Entropy Transfer

Entropy is transferred only by heat or mass flow For heat transfer:

S = S = S =

For mass flow: S =

n.b. there is no entropy transfer due to work

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Generating Entropy

friction, turbulence, mixing, etc.

Ssys = Sgen + (Q/T)

Sgen = Ssys + Qsurr/Tsurr

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Sgen for Control Volumes

The rate of entropy for an open system:

dSCV/dt = (Q’/T) + m’isi – m’ese + S’gen

Special cases:

Steady flow (dSCV/dt = 0) S’gen = -(Q’/T) - m’isi + m’ese

Steady flow single stream: S’gen =

Steady flow, single stream, adiabatic: S’gen =

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Next Time

Read: 8.1-8.5 Homework: Ch 7, P: 107, 120, Ch 8, P: 22,

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