In the result of a series of experiments the relationships of blade flutter margin with rotor rotational speed,effective CG position of blade in chord and torsional stiffness of blade have been obtained.

 
  • 通過(guò)激槳葉的扭轉頻率、測槳葉的揮舞響應,試驗得到了槳葉顫振裕度與旋翼轉速、槳葉弦向有效重心位置及槳葉扭轉剛度之間的關(guān)系,即槳葉顫振裕度隨旋翼轉速的提高而降低;
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