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Low-Speed Investigation of Several Types of Split Flap on a 47.7 Degree Sweptback-Wing - Fuselage Combination of Aspect Ratio 5.1 at a Reynolds Number of 6.0 X 10(Exp 6)
| Author: | Spooner, Stanley H. |
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| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L51D20 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58811/ |
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