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Influence of airfoil trailing-edge angle and trailing-edge-thickness variation on the effectiveness of a plain flap at high subsonic Mach numbers
| Author: | Hemenover, Albert D |
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| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A51C12a |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58719/ |
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