Loading trajectory is the key factor for aircraft skin stretch forming. Initial loading traj ectory of double curve skin was designed through the analytic method.
加载轨迹是决定飞机蒙皮拉伸成形质量的关键因素。
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Stretch forming is the basic method for aircraft skin.
拉伸成形是飞机板金的基本成形方法。
Loading trajectory is the key factor for aircraft skin stretch forming.
加载轨迹是决定飞机蒙皮拉伸成形质量的关键因素。
In this paper, the pre and post process system (POPPS) for stretch forming simulation with FEM is presented.
介绍了飞机蒙皮拉形过程有限元分析软件的前后置处理系统POPPS。
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