1.

Which of the following is the correct lift balancing equation for thrust producing engines?

A. L=Wcos <sub>2</sub>
B. L=Wsin <sub>2</sub>
C. L= ( frac{cos gamma _2}{W} )
D. L= ( frac{sin gamma_2}{W} )
Answer» B. L=Wsin <sub>2</sub>


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