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The effects of Reynolds number at Mach numbers up to 0.94 on the loading on a 35 degree swept-back wing having NACA 65(1)A012 streamwise sections
| Author: | Tinling, Bruce E. |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A52B20 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59190/ |
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