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Flight Investigation at Mach Numbers From 0.67 to 1.81 of the Longitudinal Stability and Control Characteristics of a 60 Degree Delta-Wing Missile Configuration Having an All-Movable Tail
| Author: | Moul, Martin T. |
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| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L53G29 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59766/ |
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