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Aerodynamic Characteristics of a 42 Degree Swept-Back Wing With Aspect Ratio 4 and NACA 64(Sub 1)-112 Airfoil Sections at Reynolds Numbers From 1,700,000 to 9,500,000
| Author: | Neely, Robert H. |
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| Year: | 1947 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L7D14 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58024/ |
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