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Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effect of sideslip on aerodynamic characteristics at a Mach number of 1.4 with the wing twisted and cambered
| Author: | Lessing, Henry C. |
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| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A50F09 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58507/ |
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