摘要: This report presents the results of a 13-flight evaluation of modifications proposed for USAF F/RF-4 longitudinal control feel systems. The modified system (phase II) consisted of a mechanical stop in place of the viscous damper, ... 展开
作者 | Keith, L. A. Marrett, G. J. Rickard, R. R. | ||
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原报告号 | AD8241481 | 总页数 | 98 |
主办者 | Non Paid Delimited ADS | ||
报告分类号 | [51C - Aircraft] | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Jet fighters Flight control systems Pitch(Motion) Oscillation Stability Maneuverability Control Damping Resonant frequency Control sticks Flight testing Angle of attack Airspeed Takeoff Approach Aircraft landings Reconnaissance aircraft Handling F-4 aircraft |