fluid_mechanics
620 Chapter 11 ■ Compressible Flow For this example, or so that By using the value from Eq. 1 and Fig. D.2, we get and f 1/ 2 / 1 2 D f 1/* / 12 D 10.02211 m2 0.1 m 0.4 f 1/* / 22 D f 1/* / 2 2 0.2 D Ma 2 0.70 p 2 p* 1.5 f 1/* / 22 D (1) (Ans) (2) We obtain p 2 from p 2 a p 2 p* b ap* p 1 b a p 1 p 0,1 b 1p 0,1 2 where p 2p* is given in Eq. 2 and p*p 1 , p 1p 0,1 , and p 0,1 are the same as they were in Example 11.12. Thus, p 2 11.52 a 1 1.7 b 10.7623101 kPa1abs24 68.0 kPa1abs2 (Ans) COMMENT A larger back pressure [68.0 kPa1abs2] than the one associated with choked flow through a Fanno duct [45 kPa1abs2] will maintain the same flowrate through a shorter Fanno duct with the same friction coefficient. The flow through the shorter duct is not choked. It would not be possible to maintain the same flowrate through a Fanno duct longer than the choked one with the same friction coefficient, regardless of what back pressure is used. Rayleigh flow involves heat transfer with no wall friction and constant cross-sectional area. 11.5.2 Frictionless Constant Area Duct Flow with Heat Transfer (Rayleigh Flow) Consider the steady, one-dimensional, and frictionless flow of an ideal gas through the constant area duct with heat transfer illustrated in Fig. 11.21. This is Rayleigh flow. Application of the linear momentum equation 1Eq. 5.222 to the Rayleigh flow through the finite control volume sketched in Fig. 11.21 results in 01frictionless flow2 or p 1 A 1 m # V 1 p 2 A 2 m # V 2 R x p 1rV22 constant (11.110) r Use of the ideal gas equation of state 1Eq. 11.12 in Eq. 11.110 leads to p 1rV22 RT constant (11.111) p Since the flow cross-sectional area remains constant for Rayleigh flow, from the continuity equation 1Eq. 11.402 we conclude that rV constant For a given Rayleigh flow, the constant in Eq. 11.111, the density–velocity product, rV, and the ideal gas constant are all fixed. Thus, Eq. 11.111 can be used to determine values of fluid temperature corresponding to the local pressure in a Rayleigh flow. To construct a temperature–entropy diagram for a given Rayleigh flow, we can use Eq. 11.76, which was developed earlier from the second T ds relationship. Equations 11.111 and 11.76 can be solved simultaneously to obtain the curve sketched in Fig. 11.22. Curves like the one in Fig. 11.22 are called Rayleigh lines. Frictionless and adiabatic converging–diverging duct Semi-infinitesimal control volume Frictionless duct with heat transfer Flow D = constant Section (1) Finite control volume Section (2) F I G U R E 11.21 Rayleigh flow.
11.5 Nonisentropic Flow of an Ideal Gas 621 T ( ) Ma b = √ 1_ k b Ma < 1 a (Ma a = 1) Ma > 1 s F I G U R E 11.22 Rayleigh line. E XAMPLE 11.15 Frictionless, Constant Area Compressible Flow with Heat Transfer (Rayleigh Flow) GIVEN Air 1k 1.42 enters [section 112] a frictionless, constant flow cross-sectional area duct with the following properties (the same as in Example 11.11): T 0 518.67 °R T 1 514.55 °R p 1 14.3 psia FIND For Rayleigh flow, determine corresponding values of fluid temperature and entropy change for various levels of downstream pressure and plot the related Rayleigh line. SOLUTION To plot the Rayleigh line asked for, use Eq. 11.111 p 1rV22 RT constant p and Eq. 11.76 s s 1 c p ln T R ln p (2) T 1 p 1 to construct a table of values of temperature and entropy change corresponding to different levels of pressure downstream in a Rayleigh flow. Use the value of ideal gas constant for air from Table 1.7 R 1716 1ft # lb21slug # °R2 or in EE system units R 53.3 1ft # lb21lbm # °R2 and the value of specific heat at constant pressure for air from Example 11.11, namely, c p 187 1ft # lb21lbm # °R2 Also, from Example 11.11, rV 16.7 lbm1ft 2 # s2. For the given inlet [section 112] conditions, we get RT 1 353.3 1ft # lb21lbm # °R241514.55 °R2 p 1 14.3 psia 1144 in. 2 ft 2 2 13.3 ft 3 lbm Thus, from Eq. 1 we get p 1rV22 RT 14.3 psia 316.7 lbm1ft 2 # s24 2 113.3 ft 3 lbm2 p 14.3 psia 3720 lbm1ft # s 2 2 constant (1) or, since 32.22 lbft 2 , p 1rV22 RT 14.3 psia 31372032.22lbft 2 411 ft 2 144 in. 2 2 p 15.10 psia constant (3) With the downstream pressure of p 13.5 psia, we can obtain the downstream temperature by using Eq. 3 with the fact that Hence, from Eq. 3, or 1rV2 2 R p 1 lbm1ft # s 2 2 31132.221lb # s 2 ft241ft # s 2 2 11 316.7 lbm 1ft 2 # s24 2 353.3 1ft # lb21lbm # °R24 1144 in. 2 ft 2 2 13.5 psia 7.65 3lbm1ft # s 2 24°R 31 lb132.2 lbm # fts 2 24 0.238 1lbft 2 2°R11 ft 2 144 in. 2 2 1.65 10 3 1lbin. 2 2°R 13.5 psia 31.65 10 3 1lbin. 2 2°R4 T 15.10 psia T 969 °R From Eq. 2 with the downstream pressure p 13.5 psia and temperature T 969 °R we get s s 1 3187 1ft # lb21lbm # 969 °R °R24 ln a 514.55 °R b 13.5 psia 353.3 1ft # lb21lbm # °R24 ln a 14.3 psia b s s 1 121 1ft # lb21lbm # °R2 By proceeding as outlined above, we can construct the table of values shown below and graph the Rayleigh line of Fig. E11.15.
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11.5 Nonisentropic Flow of an Ideal Gas 621<br />
T<br />
( )<br />
Ma b =<br />
√ 1_ k<br />
b<br />
Ma < 1<br />
a (Ma a = 1)<br />
Ma > 1<br />
s<br />
F I G U R E 11.22<br />
Rayleigh line.<br />
E XAMPLE 11.15<br />
Frictionless, Constant Area Compressible Flow<br />
with Heat Transfer (Rayleigh Flow)<br />
GIVEN Air 1k 1.42 enters [section 112] a frictionless, constant<br />
flow cross-sectional area duct with the following properties<br />
(the same as in Example 11.11):<br />
T 0 518.67 °R<br />
T 1 514.55 °R<br />
p 1 14.3 psia<br />
FIND For Rayleigh flow, determine corresponding values of<br />
<strong>fluid</strong> temperature and entropy change for various levels of downstream<br />
pressure and plot the related Rayleigh line.<br />
SOLUTION<br />
To plot the Rayleigh line asked for, use Eq. 11.111<br />
p 1rV22 RT<br />
constant<br />
p<br />
and Eq. 11.76<br />
s s 1 c p ln T R ln p (2)<br />
T 1 p 1<br />
to construct a table of values of temperature and entropy change<br />
corresponding to different levels of pressure downstream in a<br />
Rayleigh flow.<br />
Use the value of ideal gas constant for air from Table 1.7<br />
R 1716 1ft # lb21slug # °R2<br />
or in EE system units<br />
R 53.3 1ft # lb21lbm # °R2<br />
and the value of specific heat at constant pressure for air from Example<br />
11.11, namely,<br />
c p 187 1ft # lb21lbm # °R2<br />
Also, from Example 11.11, rV 16.7 lbm1ft 2 # s2. For the<br />
given inlet [section 112] conditions, we get<br />
RT 1<br />
353.3 1ft # lb21lbm # °R241514.55 °R2<br />
p 1 14.3 psia 1144 in. 2 ft 2 2<br />
13.3 ft 3 lbm<br />
Thus, from Eq. 1 we get<br />
p 1rV22 RT<br />
14.3 psia 316.7 lbm1ft 2 # s24 2 113.3 ft 3 lbm2<br />
p<br />
14.3 psia 3720 lbm1ft # s 2 2 constant<br />
(1)<br />
or, since<br />
32.22 lbft 2 ,<br />
p 1rV22 RT<br />
14.3 psia 31372032.22lbft 2 411 ft 2 144 in. 2 2<br />
p<br />
15.10 psia constant<br />
(3)<br />
With the downstream pressure of p 13.5 psia, we can obtain<br />
the downstream temperature by using Eq. 3 with the fact that<br />
Hence, from Eq. 3,<br />
or<br />
1rV2 2 R<br />
p<br />
1 lbm1ft # s 2 2 31132.221lb # s 2 ft241ft # s 2 2 11<br />
316.7 lbm 1ft 2 # s24 2 353.3 1ft # lb21lbm # °R24<br />
1144 in. 2 ft 2 2 13.5 psia<br />
7.65 3lbm1ft # s 2 24°R 31 lb132.2 lbm # fts 2 24<br />
0.238 1lbft 2 2°R11 ft 2 144 in. 2 2<br />
1.65 10 3 1lbin. 2 2°R<br />
13.5 psia 31.65 10 3 1lbin. 2 2°R4 T 15.10 psia<br />
T 969 °R<br />
From Eq. 2 with the downstream pressure p 13.5 psia and temperature<br />
T 969 °R we get<br />
s s 1 3187 1ft # lb21lbm #<br />
969 °R<br />
°R24 ln a<br />
514.55 °R b<br />
13.5 psia<br />
353.3 1ft # lb21lbm # °R24 ln a<br />
14.3 psia b<br />
s s 1 121 1ft # lb21lbm # °R2<br />
By proceeding as outlined above, we can construct the table of<br />
values shown below and graph the Rayleigh line of Fig. E11.15.