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

Which of the following is the correct lift balancing equation for thrust producing engines? Correct Answer L=Wcosγ2

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