摘要: An investigation has been made of a 450 sweptback cambered wing in combination with an unindented body and a body symmetrically indented with respect to its axes designed for a Mach number of 1.2. The ratio of body frontal area to... 展开
作者 | Patterson, J. C. Loving, D. L. | ||
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原报告号 | N19980223585 | 总页数 | 38 |
主办者 | National Aeronautics and Space Administration | ||
报告分类号 | [51A - Aerodynamics51C - Aircraft] | ||
报告类别/文献类型 | DE / NTIS科技报告 | ||
关键词 | Body-wing configurations Lift drag ratio Indentation Cambered wings Airfoil profiles Sweptback wings Wing planforms Zero lift Wave drag Asymmetry Reynolds number Mach number |