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Measurements of Aerodynamic Characteristics of a 35 Degree Sweepback NACA 65-009 Airfoil Model With 1/4 Chord Flap Having 31 Percent Flap Chord Overhang Balance by the NACA Wing Flow Method
| Author: | Johnson, Harold I. |
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| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L50H09 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58536/ |
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