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# Question

Fundamentals-of-Compressible-Fluid-Dynamics
Balachandra
Chapter 3
7. Air at 3 bar and 300 K
enters a duct of varying cross-sectional area of 150m/s. at inlet
scetion the area is 0.05 m2. At another section downstream of it,
the fluid properties are 2 bar and 280K with a flow velocity of
250m/s, Assuming air to be perfect gas, find the internal thrust
produced. H

[Ans. -1586.74 N]

8. The entry conditions of air into horizontal
duct are 300K 345kPa and 150 m/s the air leaves the duct at 277K,
205.8K and 260m/s. The area at entry is 0.05m2. Assuming adiabatic
flow, find (i) stagnation temperature (ii) mass flow rate (iii)
maximum velocity and (iv) area at exit
[To1 =311.15K; To2 =310.7K; m=30kg/s;Vmax=790m/s;
A2=0.0445m2]
9. Determine the velocity of air corresponding, a velocity
temperamre of 1C.

[Ans. V = 742.12 m/s]
10. Air at stagnation conditions has a
temperature of 800 K. Determine the velocity of sound and maximum
possible velocity. What is the velocity of sound when the flow is
at half the maximum velocity.

[Ans. (i) a0 = 567 m/s; Vmax = 1265 m/s
(ii) a = 491 m/s]

11. A perfect gas having Cp = 1017.4 J/kg
K and molecular weight 28.97 flows adiabatically in a converging
passage with a mass flow rate of 29.180 kg/s. At a particular
location, M = 0.6, T= 550 K and p = 2 x
105 N/m2. Calculate the area of cross-section of the duct at the
location.

[Ans. A = 0.08167 m2]

PLEASE SOLVE ALL QUESTION TOMORROW IS MY EXAM OTHERWISE
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