kaperry
kaperry
25.02.2020 • 
Engineering

Air enters the combustor of a jet engine at P1 = 10 atm, T1 = 1000oR, and M1 = 0.2. Fuel is injected and burned, with a fuel-air ratio (by mass) of 0.06. The heat released during the combustion is 4.5 × 108 ft-lb/slug of fuel. Assuming one-dimensional frictionless flow with γ = 1.4 for the fuel-air mixture, calculate M2, P2, and T2 at the exit of the combustor

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