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.

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It functions as a technical support for the research of stretch forming process over reconfigurable tooling.

本系统的建立,为可重构柔性模具蒙皮拉形工艺研究提供了技术保障.

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These results provide significant guidance to the practical application of multi - point stretch - forming technique for skin parts.

研究结果对蒙皮件多点拉形技术的实际应用具有一定的参考价值.

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