If this load centroid is behind the elastic axis of the wing structure, then a nose-down twist of the main wing surface results . 如果该载荷重心在机翼结构弹性轴之后,则引起主机翼表面前端向下的扭转。
Layout optimization of aircraft wing with topology shaping sizing variables all considered 基于杂交算法的机翼结构布局优化设计
Multi - objective optimization design of wing structure with the model management framework 基于模型管理框架的机翼结构多目标优化设计
The frame - change law of space - time and the response functionals of simple materials with internal constraints 基于仿生的大展弦比机翼结构布局形式研究