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Which of the following is the correct lift balancing equation for thrust producing engines?(a) L=Wcosγ2(b) L=Wsinγ2(c) L=\(\frac{cos\gamma _2}{W}\)(d) L=\(\frac{sin\gamma_2}{W}\)I got this question in class test.Question is from Climb and Descent Performance with Thrust-Producing Engines in chapter Climb and Descent Performance of Aircraft Performance

Answer»

The CORRECT answer is (a) L=Wcosγ2

Explanation: The correct lift BALANCING equation for THRUST PRODUCING engines is given by the equation L=Wcosγ2 where L is lift, W is weight and γ is the angle at which the FORCE is acting on the aircraft.



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