摘要: Force and moment characteristics were measured for two trapezoidal oblique wings and a conventional swept wing mounted on a body of revolution at Mach numbers from 0.2S to 2.0. Both oblique wings had the same planform, but differe... 展开
作者 | Edward J. Hopkins Sam C. Yee | ||
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原报告号 | NASA-TM-X-3547 | 总页数 | 485 |
主办者 | National Aeronautics and Space Administration | ||
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Oblique wing - Swept wing - Wing flexibility - Wing flow separation |