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Wind-tunnel tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds: wing and fuselage pressure distribution
| Author: | Cleary, Joseph W. |
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| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A50D07 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58501/ |
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