摘要: A flight test investigation was conducted to evaluate the feasibility of an aerodynamic spoiler system installed on a Piper PA-30 airplane for deterring stall, and to determine its possibilities as a stall deterrent for other ligh... 展开
作者 | H. L. Chevalier | ||
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原报告号 | ADA006995 | 总页数 | 80 |
主办者 | Department of Transportation Federal Aviation Administration Aircraft Development Service | ||
报告分类号 | [51B - Aeronautics, 85D - Transportation Safety] | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Aviation safety Spoilers Flight testing Stalling Spinning(Motion) Aviation accidents Prevention Feasibility studies Test methods Center of gravity Level flight Climbing Descent Turning flight Flaps(Control surfaces) Airplanes Stall deterrence Spin deterrence DOT/4DZ/DA DOT/5A |