MCQOPTIONS
Saved Bookmarks
| 1. |
The magnus effect is defined as: |
| A. | The generation of lift per unit drage force |
| B. | The circulation induced in an aircraft wing |
| C. | The separation of boundary layer near the trailing edge of a slender body |
| D. | The generation of lift on a rotating cylinder in a uniform flow. |
| Answer» E. | |