Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Effects of split flaps, elevons, and leading-edge devices at low speed
| Author: | Hopkins, Edward J. |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A9C21 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58259/ |