aircraft skin meaning in Chinese
飞行器外壳, 飞机蒙皮
航空器蒙皮
Examples
- Research on algorithm of aircraft skin defect recognition through magneto optic image
飞机蒙皮缺陷磁光图像识别算法研究 - In approximately 1 minute at those temperatures the aircraft skin will be breached
大约一分钟内，这样的高温将把飞机外壳破坏。 - The result was shown that the program runs quickly and in reliability , it can replace the nomograph method and use easily for predicating sonic fatigue life of aircraft skin - panel structure
通过已有的算例进行验证，结果表明计算迅速可靠，可以代替以列线图为主要手段的求解方法，广泛的应用于工程领域。 - In first part of the thesis , by a review of the research on aircraft sonic fatigue , the formulas for calculating natural frequencies of the typical aircraft skin - panel structure with four edges simply - supported or four edges fixed - supported were drawn , the response of displacement and stress was analysed under the condition of random white noise loading with the steady - state or unsteady - state . the procedure how to use data of s - n curve under constant loading for predicating the fatigue life of skin - panel subjected to random loading was shown
通过对声疲劳问题研究的回顾，根据典型飞机蒙皮壁板模型，整理了四边固支，四边简支两种边界条件下多阶模态固有频率，非平稳及平稳随机白噪声载荷下的位移和应力响应，以及如何从等幅s ? n曲线求得随机载荷应力下的疲劳寿命。 - From the postulate of the stretch - forming , with the help of sheet - forming software , the computer simulation of the stretch - forming of a s - shape aircraft skin is proposed in this paper , including the build of fem mode , the preferences of simulation , the forming , the whole body spring back and the spring back after clipping . the spring back radius is calculated on the simulate results and contrasted with the reality
从拉形的基本原理出发，本文运用sheet - forming对s形飞机蒙皮进行拉形成形的计算机仿真，包括有限元模型的建立、仿真参数的选择、加载成形、整体卸载回弹、切边卸载回弹；运用仿真结果计算回弹半径求出回弹量，并将分析计算结果与实际生产的回弹量对比。