摘要: The test objective was to evaluate the performance and flying qualities of the F-4E aircraft equipped with the two-position leading edge slat and to obtain data necessary to update the F-4 Flight Manual. The two-position slat test... 展开
作者 | Boxwell, B. R. Hubenet, R. C. Powell, C. W. | ||
---|---|---|---|
原报告号 | AD9042870 | 总页数 | 295 |
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 Leading edge flaps Modification kits Maneuverability Angle of attack Turning flight Airspeed Degradation Performance(Engineering) Acceptability Hydraulic actuators Extendable structures Flight testing Attitude control systems Flight instruments Acceleration Stability Aerodynamic loading Takeoff Instruction manuals Load distribution Transonic flight Approach Roll F-4e aircraft Leading edge slats F-4 aircraft Modification |