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An investigation at Mach numbers of 1.40 and 1.59 of the effects of aileron profile on the aerodynamic characteristics of a complete model of a supersonic aircraft configuration
| Author: | Spearman, M. Leroy |
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| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L50J31 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58682/ |
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