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
其它零部件传递的集中载荷和空气气动载荷外,还要承受航炮发
时的冲击力,整个结构始终处于不规则的振动状态。
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
其它零部件传递的集中载荷和空气气动载荷外,还要承受航炮发
时的冲击力,整个结构始终处于不规则的振动状态。
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
自由尾迹模型,本文在第三章建立了一个适合于直
尾迹结构及桨-涡干扰气动特性分析的方法和模型。
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