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Reduction of profile drag at supersonic velocities by the use of airfoil sections having a blunt trailing edge
| Author: | Chapman, Dean R. |
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| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A9H11 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58400/ |
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