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Modern Engineering Thermodynamics

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Problems 691<br />

A plot of this function is called the Fanno line for the flow. Plot<br />

T out vs. _Sp/ ð _mc v Þ for air using 0 ≤ T out ≤ T in : Take T os = 300 K and<br />

T in = 290 K. Note that _Sp/ ð _mc v Þ is double valued in T out and its<br />

maximum value occurs at M = 1:0: Determine the two values of<br />

T out for which _S p = 0 when T os = 300 K and T in = 290 K.<br />

81.* Rayleigh line. An analysis of the frictionless aergonic flow of an<br />

ideal gas with constant specific heats traveling through a constant<br />

area duct with heat transfer at the walls can be carried out by<br />

combining the continuity equation and the linear momentum<br />

rate balance equation to yield the following set of equations:<br />

p out<br />

p in<br />

= 1 + kM2 in<br />

1 + kM 2 out<br />

2<br />

× 1 + kM2 in<br />

T out<br />

T in<br />

= M out<br />

M in<br />

1 + kM 2 out<br />

ðT os Þ out<br />

= M out<br />

ðT os Þ in<br />

M in<br />

2<br />

1 + kM in<br />

×<br />

1 + kM out<br />

1 + k − 1<br />

2 M2 out<br />

1 + k − 1<br />

2 M2 in<br />

and Eq. (7.37) gives s out = s in + c p ln ðT out /T in Þ− R ln ðp out /p in Þ:<br />

For air, with (T os ) in = 100°C, p in = 0.5 MPa, M in = 0.5,<br />

and s in = 2.2775 kJ/(kg· K), generate the following plots for<br />

0 ≤ M out ≤ 10:<br />

a. T out vs. s out (this plot is called the Rayleigh line).<br />

<br />

<br />

b. _Q / _m = c p ðT os Þ out<br />

− ðT os Þ in vs: Mout (this is the heat transfer<br />

per unit mass to or from the air).<br />

<br />

c. _S p / _mc p =<br />

Q<br />

ð sout − s in Þ/c p − _ / _m<br />

vs: M out,<br />

cpTw<br />

where T w = 1 2<br />

ð T in + T out Þ is the mean wall temperature. Note<br />

that s out is a maximum when M out = 1.0.

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