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Modern Engineering Thermodynamics

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9.9 Unsteady State Processes in Open Systems 305<br />

CASE STUDY 9.2. HYDRODYNAMIC FLOW SYSTEMS<br />

A variety of hydrodynamic flow situations can be effectively<br />

analyzed with the entropy rate balance. Consider a steady state,<br />

steady flow, single-inlet, single-outlet system. The MERB for this system<br />

using the definition of enthalpy, h = u + pv, and the definition<br />

of density, ρ =1/v, can be written as<br />

<br />

_Q − _W = _m u 2 − u 1 + ðp/ρÞ 2<br />

− ðp/pÞ 1<br />

+ V2 2 − <br />

V2 1 /2gc + ðg/g c ÞðZ 2 − Z 1 Þ<br />

<br />

<br />

= _m u 2 − u 1 − ðg/g C Þ 1 ðh L Þ 2<br />

where, using the specific weight γ = ρg,<br />

1 h L Þ 2<br />

= ðpg c /γÞ 1<br />

− ðpg c /γÞ 2<br />

+ V1 2 − V 2 2 <br />

/2g + Z1 − Z 2 (9.52)<br />

is the head loss between the inlet station 1 and the exit station 2. In<br />

fluid mechanics texts, Eq. (9.52) is known as the Bernoulli equation,<br />

named after the Swiss mathematician and hydrodynamist Daniel<br />

Bernoulli (1700–1782). The MSRB for this system is<br />

_S P = _m ðs 2 − s 1 Þ− _Q /T b<br />

If the flowing fluid is a constant specific heat incompressible liquid,<br />

ρ 1 = ρ 2 = constant<br />

u 2 − u 1 = cT ð 2 − T 1 Þ<br />

s 2 − s 1 = c ln T 2<br />

T 1<br />

and, if it is a constant specific heat ideal gas,<br />

ρ = p/ ðRTÞ = 1/v<br />

u 2 − u 1 = c v ðT 2 − T 1 Þ<br />

s 2 − s 1 = c p ln T 2<br />

T 1<br />

− R ln p 2<br />

p 1<br />

Now, let us compare the rate of entropy production for two cases (i.e.,<br />

two thermodynamic paths), adiabatic flow and isothermal flow.<br />

Case A. SS, SF, SI, SO, aergonic, adiabatic flow 8<br />

Incompressible, constant specific heat liquids. In this case, the<br />

MERB gives<br />

<br />

T 2 = T 1 + g 1 ðh L Þ 2 / ð cgc Þ<br />

Ideal gases with constant specific heats. In this case, the MERB<br />

gives<br />

<br />

T 2 = T 1 + g 1 h L Þ 2 / ð cv g c Þ<br />

and the MSRB gives<br />

<br />

_S p<br />

P ideal = _mc p ln 1 + g 1 ðh L Þ 2 / ð cv g c T 1 Þ − _mR 2 ln (9.54)<br />

gas<br />

p 1<br />

<br />

ðadiabaticÞ<br />

Case B. SS, SF, (SI, SO) aergonic, isothermal flow<br />

Incompressible, constant specific heat liquids. In this case, the<br />

MERB gives<br />

and the MSRB gives<br />

<br />

_S P <br />

<br />

_Q = − _mg 1 h L Þ 2 /gc<br />

incomp:<br />

liquid<br />

ðisothermalÞ<br />

<br />

= _mg 1 h L Þ 2 /ðTb g c Þ<br />

(9.55)<br />

Ideal gases with constant specific heats. In this case, the MERB<br />

again gives<br />

and the MSRB gives<br />

<br />

_S P ideal<br />

gas<br />

<br />

ðisothermalÞ<br />

<br />

_Q = − _mg 1 h L Þ 2 /gc<br />

<br />

= _mg 1 ðh L Þ 2 /ðTb g c Þ − _mRln p 2<br />

(9.56)<br />

p 1<br />

The question is this: Which process, adiabatic or isothermal, is the<br />

more efficient by producing less entropy? For the incompressible<br />

liquids, we must compare Eqs. (9.53) and (9.55). Using a series<br />

expansion for the logarithm, we find that, for all x > 0, ln(l + x) < x,<br />

so that for T b = T l , we have<br />

<br />

c ln 1 + g 1 ðh L Þ 2 / ð cgc T 1 Þ < g 1 ðh L Þ 2 / ð T1 g c Þ<br />

and, consequently,<br />

<br />

_S P <br />

incomp:<br />

liquid<br />

ðadiabaticÞ<br />

<br />

< _S P <br />

incomp:<br />

liquid<br />

ðisothermalÞ<br />

Similarly, for the ideal gases, we compare Eqs. (9.54) and (9.56) and<br />

again find that.<br />

<br />

_S <br />

P ideal < _S P ideal<br />

gas<br />

gas<br />

<br />

<br />

ðadiabaticÞ<br />

ðisothermalÞ<br />

and the MSRB gives<br />

<br />

_S<br />

incomp: P<br />

liquid:<br />

ðadiabaticÞ<br />

<br />

= _mc ln 1 + g 1 h L Þ 2 / ð cgc T 1 Þ<br />

(9.53)<br />

In both of these cases, the adiabatic process produces less entropy.<br />

This is always true in this type of comparison, because an adiabatic<br />

system eliminates the entropy production due to heat transfer across<br />

the system boundary.<br />

(Continued )

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