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Pressure Distribution and Damping in Steady Pitch at Supersonic Mach Numbers of Flat Swept-Back Wings Having All Edges Subsonic
| Author: | Walker, Harold J. |
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| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2197 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55589/ |
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