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The Effects of Circular End Plates on the Lift, Drag, and Pitching Moment at Subsonic and Supersonic Speeds on a Modified Triangular Wing Having an Aspect Ratio of 2, a Taper Ratio of 0.33, and a 45 Degree Swept Leading Edge
| Author: | Petersen, Robert B. |
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| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A53J14 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60547/ |
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