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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 |
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| Year: | 1948 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A8D20 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57732/ |
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