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A Summary of the Longitudinal and Lateral Stability and Control Characteristics Obtained From Rocket-Model Tests of a Swept-Wing Fighter-Type Airplane at Mach Numbers From 0.5 to 1.9
| Author: | Mitcham, Grady L. |
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| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L56K19 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc53053/ |
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