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An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degree Sweepback: Stability and Control Characteristics at a Mach Number of 1.61 of the Complete Configuration Equipped With Spoilers
| Author: | Hamilton, Clyde V. |
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| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L54F15 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60539/ |
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