Strength Of Materials
2) (11 pts each) Consider an ideal Jet-Propulsion Cycle. At the inlet to the diffuser the pressure is 40 kPa and the temperature is -30°C and the air velocity is V1 = (700 + 3y) m/s. (That is, if y = 12, then V1 = 736 m/s). Use a cold-air standard (constant specific heats). The pressure ratio across the compressor is 8. The maximum temperature for the cyde is 1450°C. Find the:
a. Temperature just after the diffusor.
b. The heat addition in the combustion chamber (or heat exchang er)
. Find the velocity at the exit of the nozzle.
c. Find the temperature at the exit of the turbine.
Getting answers to your urgent problems is simple. Submit your query in the given box and get answers Instantly.