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Effect of Reduction in Thickness From 6 to 2 Percent and Removal of the Pointed Tips on the Subsonic Static Longitudinal Stability Characteristics of a 60-Degree Triangular Wing in Combination With a Fuselage
| Author: | Palmer, William E. |
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| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L53F24 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59786/ |
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