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Free-Flight Investigation of Fullspan, 0.2 Chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Wing Sweepback, Taper, Aspect Ratio, and Section-Thickness Ratio
| Author: | Sandahl, Carl A. |
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| Year: | 1947 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L7F30 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58097/ |
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