タイトル | Aerodynamic tailoring of the Learjet Model 60 wing |
著者(英) | Madson, Michael D.; Hawke, Veronica M.; Kennelly, Robert A., Jr.; Hinson, Michael L.; Chandrasekharan, Reuben M. |
著者所属(英) | NASA Ames Research Center |
発行日 | 1993-01-01 |
言語 | eng |
内容記述 | The wing of the Learjet Model 60 was tailored for improved aerodynamic characteristics using the TRANAIR transonic full-potential computational fluid dynamics (CFD) code. A root leading edge glove and wing tip fairing were shaped to reduce shock strength, improve cruise drag and extend the buffet limit. The aerodynamic design was validated by wind tunnel test and flight test data. |
NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
レポートNO | 95A89194 SAE PAPER 932534 |
権利 | Copyright |
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