摘要: An experimental investigation was conducted to assess the effect of surface finish on the longitudinal and lateral aerodynamic characteristics of a highly-swept wing at supersonic speeds. A study of the effects of wing dihedral wa... 展开
作者 | Darden, C. M. | ||
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原报告号 | N8925117 | 总页数 | 88 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Dihedral angle Lift drag ratio Milling (Machining) Supersonic speed Surface roughness effects Swept wings Aerodynamic drag Angle of attack Grooves Lateral stability Longitudinal stability Mach number Reynolds number Wind tunnel tests Wing profiles |