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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 |
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Answer» The CORRECT answer is (a) L=Wcosγ2 |
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