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Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-Wing Airplane Configuration Equipped With a Canard Control and With Wing Trailing-Edge Flap Controls
| Author: | Spearman, M. Leroy |
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| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L58A20 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63755/ |
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