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Flight Mechanics MCQ
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Which of the following is the correct expressio...
Which of the following is the correct expression for Lift (L)?
A. L = 0.5 * ρ * V² * S * CL
B. L = m * g
C. L = T – D
D. L = P * V
Explanation:
The lift equation is L = 0.5 * ρ * V² * S * CL, where CL is lift coefficient.
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Flight Mechanics MCQ
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