Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
在飞
飞行过程中,炮舱结构除承受飞
其它零部件传递
集中载荷和空气气动载荷外,还要承受航炮发
时
冲击力,整个结构始终处于不规则
振动状态。
载重量;飞


空气动力负荷Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
在飞
飞行过程中,炮舱结构除承受飞
其它零部件传递
集中载荷和空气气动载荷外,还要承受航炮发
时
冲击力,整个结构始终处于不规则
振动状态。
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基于桨叶二阶
力线理论和旋
自由尾迹模型,本文在第三章建立了一个适合于

旋
尾迹结构及桨-涡干扰气动特性分析
方法和模型。
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