MCQOPTIONS
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MCQOPTIONS
| 1. |
The total drag coefficient for a wing is given by______ |
| A. | c<sub>d</sub>= ( frac {D_f+D_P+D_i}{Sq_ } ) |
| B. | C<sub>d</sub>= ( frac {D_f+D_P}{Sq_ } ) |
| C. | C<sub>d</sub>= ( frac {D_f+D_P+D_i}{Sq_ } ) |
| D. | C<sub>d</sub>= ( frac {D_f+D_P}{Sq_ } )+D<sub>i</sub> |
| Answer» D. C<sub>d</sub>= ( frac {D_f+D_P}{Sq_ } )+D<sub>i</sub> | |