摘要: The Symposium was organized because of the continuing need for design data and principles relevant to the flight of aircraft and missiles at high angles of attack and the substantial efforts devoted to vehicles capable of controll... 展开
原报告号 | ADA067323 | 总页数 | 548 |
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报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Flight control systems Aerodynamic control surfaces Angle of attack Aerodynamic characteristics Aerodynamic configurations Air intakes Mathematical models Aerodynamic stability Flow separation Three dimensional flow Strakes Vortices Symposia Meetings NATO furnished Unsteady flow |