摘要: The CH-47C was flight tested to obtain detailed performance data and to verify compliance of the aircraft with the manufacturer's detail specification and applicable military specifications. The test results show that the helicopt... 展开
| 作者 | Forsyth, R. F. Nagata, J. I. Marr, G. A. Burden, J. R. | ||
|---|---|---|---|
| 原报告号 | AD892400 | 总页数 | 144 |
| 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 | Helicopters Performance(Engineering) Flight testing Specifications Acceptability Gas turbines Helicopter engines Cockpits Vibration Torque Aerodynamic characteristics Aircraft noise Hovering Climbing Airspeed Cargo Payload Load distribution Human factors engineering Pilots Handling Flight control systems Aerodynamic loading Flight instruments Display systems Ch-47c aircraft H-47 aircraft Shafts(Machine elements) Turbojet engines T-55-l-11 engines | ||
