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Maximum-Lift Investigation of a 1/40-Scale X-1 Airplane Wing at Mach Numbers From 0.60 to 1.15
| Author: | Turner, Thomas R. |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L50C28 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58601/ |
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