摘要: The longitudinal aerodynamic characteristics of a wing-body-horizontal-tail configuration designed for efficient performance at transonic speeds has been investigated at Mach numbers from 0.80 to 1.03 in the Langley 16-foot transo... 展开
作者 | West, F. E. | ||
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原报告号 | N19980223614 | 总页数 | 32 |
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 and tail configurations Aircraft design Swept wings Wind tunnel tests Transonic speed Cambered wings Aerodynamic characteristics Aerodynamic balance Mach number Reynolds number Leading edges Lift drag ratio Chords(Geometry) Aspect ratio Airfoil profiles Aerodynamic drag |