integral wing panel

基本解释

Finite element simulation of stress and strain on the incremental bend forming technology of the integral wing-skin panel;
采用逐点增量弯曲的方法对网格式带筋整体壁板进行了试验研究，并进行了有限元模拟。
With the development of integral wing panel design, conventional manufacture mode of integral panel can not satisfy modern manufacturing requirement.
随着现代机翼整体壁板设计水平的不断提高，传统的制造模式已不能满足其制造要求。
An integral wing panel is represented as feature sets, and the features are decomposed as information sets such as location, direction, geometric size, Boolean operation etc.
将整体壁板分解为特征的集合，并进一步将特征分解为特征的位置、方向、几何尺寸、布尔运算等信息的集合。