摘要: A program has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of certain wing plan-form variations on the aerodynamic characteristics of wing-body combinations at supersonic speeds. T... 展开
作者 | Sevier, J. R. | ||
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原报告号 | N19980228048 | 总页数 | 42 |
主办者 | National Aeronautics and Space Administration | ||
报告分类号 | [51A - Aerodynamics] | ||
报告类别/文献类型 | DE / NTIS科技报告 | ||
关键词 | Aerodynamic characteristics Lift drag ratio Low aspect ratio wings Reynolds number Supersonic speed Swept wings Trailing edges Wing planforms Mach number Longitudinal stability Bodies of revolution Body-wing configurations Supersonic wind tunnels Drag Aspect ratio Wings |