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Wind-tunnel investigation at Mach numbers from 0.50 to 1.29 of an unswept, tapered wing of aspect ratio 2.67 with leading- and trailing-edge flaps - leading-edge flaps deflected
| Author: | Stivers, Louis S., Jr. |
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| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A50K10 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58712/ |
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