摘要: A comprehensive set of experimental and analytical investigations have beenconducted to assess the potential aerodynamic benefits from spanwise blowing at the tip of a moderate aspect ratio, swept wing. An analytical model has bee... 展开
作者 | Mineck, R. E. | ||
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原报告号 | N9225261 | 总页数 | 359 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aerodynamic characteristics Computational fluid dynamics Drag reduction Spanwise blowing Swept wings Wing tips Computerized simulation Subsonic flow Wind tunnel tests Aspect ratio Boundary conditions Mach number Mathematical models Navier-sto |