Question: A. Calculate the specific thrust ( F / ) and the specific fuel consumption ( S ) of an ideal turbojet for the following conditions:

A. Calculate the specific thrust ( F / ) and the specific fuel consumption ( S ) of an ideal turbojet for the following conditions: M = 2.0 T = 240K P = 20,000 N / m c = 25 T = 2000 K h = heating value of fuel = 4.42 x 10 J / kg ( fuel ) Also find T, T, T, T, P, P, P, P, M, U, T, P. B. If A = 2.0 m, calculate the thrust and the fuel flow rate for this engine

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