1.

Which of the following is the correct formula for lift of an aircraft?

A. L= ( frac{1}{2} ) V<sup>2</sup>SC<sub>l</sub>
B. L= ( frac{1}{2} )V<sup>2</sup>SC<sub>l</sub>
C. L= ( frac{1}{2} ) V<sup>2</sup>C<sub>l</sub>
D. L= ( frac{1}{2} )PV<sup>2</sup>SC<sub>l</sub>
Answer» B. L= ( frac{1}{2} )V<sup>2</sup>SC<sub>l</sub>


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