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Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-Aspect-Ratio Unswept Wing and a Horizontal Tail Mounted Well Above the Wing Plane - Longitudinal Stability and Control
| Author: | Smith, Willard G. |
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| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-SA54D05 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc65414/ |
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