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
机行过程中，炮舱结构除
机其它零部件传递的集中载荷和空气气动载荷外，还要航炮发
时的冲击
，整个结构始终处于不规则的振动状态。
行时的载重量；机机翼的空气动负荷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.
在机行过程中，炮舱结构除机其它零部件传递的集中载荷和空气气动载荷外，还要航炮发时的冲击，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.
基于桨叶二阶升
论和旋翼自由尾迹模型，本文在第三章建立了一个适合于直升机旋翼尾迹结构及桨-涡干扰气动特性分析的方法和模型。
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