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Rocket-Model Investigation of the Longitudinal Stability, Drag, and Duct Performance of a 60 Degree Delta-Wing Canard Aircraft With Twin Side Inlets at Mach Numbers From 0.80 to 1.70
| Author: | Bond, Aleck C. |
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| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L53D10A |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc53133/ |
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