Subsonic non after burning engine needs to be design based on following data. Take off trust is 15000 N and bypass ratio is 1.2. Find the weight of this engine. Consider first order statistical jet engine model.

Subsonic non after burning engine needs to be design based on following data. Take off trust is 15000 N and bypass ratio is 1.2. Find the weight of this engine. Consider first order statistical jet engine model. Correct Answer 3123 unit

Given, Thrust T = 15000N, BPR = 1.2 Now, weight is given by, W = 0.084 * (T1.1)* e (-0.045*BPR). W = 0.084 * (150001.1) * e (-0.045*1.2) = 0.084*39237.4147*0.9474 = 3123 unit.

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