19.09.2019 Views

fluid_mechanics

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

598 Chapter 11 ■ Compressible Flow<br />

T<br />

p 0<br />

T 0<br />

s<br />

T 0<br />

T* =<br />

( )<br />

______ k<br />

p* =<br />

k – 1<br />

p 0<br />

______ 2<br />

( k + 1 )<br />

______ 2<br />

( k + 1 )<br />

F I G U R E 11.9 The relationship<br />

between the stagnation and critical states.<br />

For k 1.4, the nominal value of k for air, Eq. 11.61 yields<br />

a p* 0.528<br />

p 0<br />

bk1.4<br />

(11.62)<br />

Because the stagnation pressure for our converging–diverging duct example is the atmospheric pressure,<br />

p atm , the throat pressure for choked air flow is, from Eq. 11.62<br />

We can get a relationship for the critical temperature ratio, T*T 0 , by substituting Ma 1<br />

into Eq. 11.56. Thus,<br />

or for k 1.4<br />

For the duct of Fig. 11.6a, Eq. 11.64 yields<br />

p* k1.4 0.528p atm<br />

T*<br />

2<br />

T 0 k 1<br />

a T* 0.833<br />

T 0<br />

bk1.4<br />

(11.63)<br />

(11.64)<br />

The stagnation and<br />

critical states are at<br />

the same entropy<br />

level.<br />

T* k1.4<br />

0.833T atm<br />

The stagnation and critical pressures and temperatures are shown on the T–s diagram of<br />

Fig. 11.9.<br />

When we combine the ideal gas equation of state 1Eq. 11.12 with Eqs. 11.61 and 11.63, for<br />

Ma 1 we get<br />

r*<br />

a p*<br />

k1k12<br />

r 0 T* b aT 0 2<br />

b a<br />

p 0 k 1 b a k 1<br />

11k12<br />

2<br />

b a<br />

2 k 1 b<br />

For air 1k 1.42, Eq. 11.65 leads to<br />

(11.65)<br />

a r* 0.634<br />

(11.66)<br />

r 0<br />

bk1.4<br />

and we see that when the converging–diverging duct flow is choked, the density of the air at the<br />

duct throat is 63.4% of the density of atmospheric air.<br />

E XAMPLE 11.5<br />

Isentropic Flow in a Converging Duct<br />

GIVEN A converging duct passes air steadily from standard FIND Determine the mass flowrate through the duct and<br />

atmospheric conditions to a receiver pipe as illustrated in Fig. sketch temperature–entropy diagrams for situations 1a2 and 1b2.<br />

E11.5a. The throat 1minimum2 flow cross-sectional area of the converging<br />

duct is 1 10 4 m 2 . The receiver pressure is 1a2 80 kPa<br />

1abs2, 1b2 40 kPa 1abs2.

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!