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A Wind-Tunnel Investigation of the Low-Amplitude Damping in Yaw and Directional Stability of a Fuselage-Tail Configuration at Mach Numbers Up to 1.10
| Author: | Palmer, William E. |
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| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L57C15 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63317/ |
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