摘要: A series of arrow wings employing various degrees of twist and camber were tested in the Langley 4- by 4-foot supersonic pressure tunnel. Aerodynamic forces and moments in pitch were measured at a Mach number of 2.05 and at a Reyn... 展开
作者 | Carlson, H. W. | ||
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原报告号 | N19980223615 | 总页数 | 36 |
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 Supersonic speed Arrow wings Swept wings Twisted wings Cambered wings Wind tunnel tests Aerodynamic coefficients Aerodynamic configurations Aerodynamic forces Airfoil profiles Aspect ratio Chords(Geometry) Leading edges Lift Lift drag ratio Minimum drag Supersonic wind tunnels Sweep angle |