MCQOPTIONS
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MCQOPTIONS
| 1. |
The correct formula for profile drag coefficient over the finite wing is_______ |
| A. | c<sub>d</sub>= ( frac {D_f+D_P}{Sq_ } ) |
| B. | c<sub>d</sub>= ( frac {D_P}{Sq_ } ) |
| C. | c<sub>d</sub>= ( frac {D_f}{Sq_ } ) |
| D. | c<sub>d</sub>= ( frac {D_f+D_P+D_i}{Sq_ } ) |
| Answer» B. c<sub>d</sub>= ( frac {D_P}{Sq_ } ) | |