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Effects of plan form, airfoil section, and angle of attack on the pressures along the base of blunt-trailing-edge wings at Mach numbers of 1.41, 1.62, and 1.96
| Author: | Goin, Kennith L |
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| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L52D21 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59299/ |
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