tiltrotor aircraft 中文意思是什麼
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The multi - body analysis of the aeroelastic stability of the tiltrotor aircraft is presented
摘要通過多體動力學方法建立了傾轉旋翼機動力學分析模型。 -
In chapter 5, a new dynamic wake model is developed by employing the rotor free - wake method in chapter 2, and is used to investigate the curve distortion during the conversion of tiltrotor aircraft between helicopter flight conditions and airplane flight conditions
在第二章方法的基礎上，第五章建立一個傾轉旋翼動態尾跡模型，使用該模型對傾轉旋翼機傾轉過渡狀態的尾跡彎曲變形進行了研究，得出了一些結論。 -
The application of parameter space method in design of flight control system for tiltrotor aircraft
參數空間法在傾轉旋翼機飛行控制系統設計中的應用 -
Tiltrotor aircraft key technology developing research
傾轉旋翼飛機技術發展研究 -
Flight control system development for the xv - 15 tiltrotor aircraft
15傾轉旋翼飛機飛行控制系統概述 -
Numerical simulations demonstrate that the multi body analytical model can analyze the aeroelastic stability of the tiltrotor aircraft in the helicopter mode
數值計算表明：建立的多體動力學模型能夠快速分析直升機模式下傾轉旋翼機復雜的旋翼機翼氣彈耦合動力學特性。
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