Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : subsonic Mach and Reynolds number effects on the characteristics of the wing and on the effectiveness of an elevon
| Author: | Reynolds, Robert M |
|---|---|
| Year: | 1948 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A8D20 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57732/ |