PROBLEM 2: The data of supersonic nozzle with Mach number 1.8 are as follows: cross -sectional area of nozzle throat is 1000 cm2, pressure in the test section is 0.7bar.Ambient pressure 101325pa and ambient temperature is 311k.Calculate
a) Cross-sectional area of test section
b) Temperature of air in the test section
SOLUTION:
