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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> | |