摘要: A limited series of stability tests were conducted by a USAF team on an F-4E equipped with fixed wing leading edge slats and an over-balanced longitudinal control system. The purpose was to evaluate the status of longitudinal stab... 展开
作者 | rutan, elbert l. powell,cecil w. | ||
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原报告号 | AD884954 | 总页数 | 91 |
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | jet fighters flight testing control surfaces leading edgestransonic airfoils pitch(motion) leading edge flaps takeoff aircraft landings stalling maneuverability stability transonic flight roll aerodynamic configurations wings loads(forces) lift angle of attack |