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Effect of Taper Ratio on Lift, Drag, and Pitching-Moment Characteristics of Thin Wings of Aspect Ratio 3 With 53.1 Degrees Sweepback of Leading Edge at Subsonic and Supersonic Speeds
| Author: | Wetzel, Benton E. |
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| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A54J20 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60891/ |
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