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(diǎn)增量彎曲的方法對網(wǎng)格式帶筋整體壁板進(jìn)行了試驗研究，并進(jìn)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(jī)翼整體壁板設(shè)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(jìn)一步將特征分解為特征的位置、方向、幾何尺寸、布爾運(yùn)算等信息的集合。