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An Investigation of the Control Effectiveness of Tip Ailerons and Spoilers on a Low-Aspect-Ratio Trapezoidal-Wing Airplane Model at Mach Numbers From 1.55 to 2.35
| Author: | Wong, Norman D. |
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| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A57I26a |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63970/ |
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