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Pressure Coefficients at Mach Numbers from 0.60 to 0.85 for a Semispan Wing with NACA 0012-64 Section, 20-Percent-Chord Plain Aileron, and 0 Degree and 45 Degree Sweepback
| Author: | Krumm, Walter J. |
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| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A50B13 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58551/ |
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