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Free-Flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of Several Aileron Configurations on a Tapered Wing Having 42.7 Degrees Sweepback
| Author: | Sandahl, Carl A. |
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| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L8K23 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58022/ |
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