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Basics of Fluid Mechanics, 2014a

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440 CHAPTER 11. COMPRESSIBLE FLOW ONE DIMENSIONAL<br />

Rearranging equation (11.177) results in<br />

(<br />

dM 2 kM 2 1+ k − 1 )<br />

M 2<br />

M 2 = 2 4 fdx<br />

1 − M 2 (11.178)<br />

D<br />

After similar mathematical manipulation one can get the relationship for the velocity<br />

to read<br />

dU<br />

U = kM 2 4 fdx<br />

2(1− M 2 (11.179)<br />

) D<br />

and the relationship for the temperature is<br />

dT<br />

T = 1 4<br />

dc (k − 1) M 4 fdx<br />

= −k<br />

2 c 2(1− M 2 (11.180)<br />

) D<br />

density is obtained by utilizing equations (11.179) and (11.170) to obtain<br />

dρ<br />

ρ = − kM2<br />

2(1− M 2 )<br />

The stagnation pressure is similarly obtained as<br />

dP 0<br />

P 0<br />

= − kM2<br />

2<br />

The second law reads<br />

( dT<br />

ds = C p ln<br />

T<br />

4 fdx<br />

D<br />

4 fdx<br />

D<br />

) ( dP<br />

− R ln<br />

P<br />

)<br />

(11.181)<br />

(11.182)<br />

(11.183)<br />

The stagnation temperature expresses as T 0 = T (1+(1− k)/2M 2 ). Taking derivative<br />

<strong>of</strong> this expression when M remains constant yields dT 0 = dT (1 + (1 − k)/2M 2 ) and<br />

thus when these equations are divided they yield<br />

dT/T = dT 0 /T 0 (11.184)<br />

In similar fashion the relationship between the stagnation pressure and the pressure can<br />

be substituted into the entropy equation and result in<br />

( ) ( )<br />

dT0<br />

dP0<br />

ds = C p ln − R ln<br />

(11.185)<br />

T 0 P 0<br />

The first law requires that the stagnation temperature remains constant, (dT 0 =0).<br />

Therefore the entropy change is<br />

ds (k − 1) dP 0<br />

= − (11.186)<br />

C p k P 0<br />

Using the equation for stagnation pressure the entropy equation yields<br />

2<br />

ds (k − 1) M<br />

=<br />

C p 2<br />

4 fdx<br />

D<br />

(11.187)

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