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Maximum-Lift Investigation at Mach Numbers From 0.05 to 1.20 of a Wing With Leading Edge Swept Back 42 Degrees
| Author: | Turner, Thomas R. |
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| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L9K03 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58344/ |
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