integral wing panel

基本解釋

Finite element simulation of stress and strain on the incremental bend forming technology of the integral wing-skin panel;
采用逐點增量彎曲的方法對網(wǎng)格式帶筋整體壁板進行了試驗研究，并進行了有限元模擬。
With the development of integral wing panel design, conventional manufacture mode of integral panel can not satisfy modern manufacturing requirement.
隨著現(xiàn)代機翼整體壁板設計水平的不斷提高，傳統(tǒng)的制造模式已不能滿足其制造要求。
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.
將整體壁板分解為特征的集合，并進一步將特征分解為特征的位置、方向、幾何尺寸、布爾運算等信息的集合。