Engineering, 11.03.2020 01:47 nan487

Air enters the combustor of a jet engine at p1=10 atm, T1=1000°R, and M1=0.2. Fuel is injected and burned, with a fuel/air mass ratio of 0.06. The heat released during combustion is 4.5 x 10^8 ft-lbf per slug of fuel (or 18,000 BTU/lbm).
1. 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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Air enters the combustor of a jet engine at p1=10 atm, T1=1000°R, and M1=0.2. Fuel is injected and b...

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