5. Consider a propeller based aircraft with a supercharger. It operates with a revolution rate of 2700 rpm, has 2 piston strokes per revolution of crankshaft, a shaft power of 100 kW, and a total...

this question is very much related to mechanical engineering. The concept of propeller and supercharger is needed

Extracted text: 5. Consider a propeller based aircraft with a supercharger. It operates with a revolution rate of 2700 rpm, has 2 piston strokes per revolution of crankshaft, a shaft power of 100 kW, and a total engine displacement of 25 L. The supercharger serves to increase the inlet pressure to the engine to sea level conditions (P1 = PsL = 101.3 kPa, pi = psL = 1.225 kg/m®). Consider an atmospheric model for air density given by Pa = Psie 5000m where h is the altitude. You may assume y = 1.4. Find the maximum altitude, h at which the engine can operate.