The goal of the the ADAPWING project is basically to achieve the same degree of wing-or, in this case turbine blade-regulation as found in hawks.
ADAPWING项目的目标，就是基本上获得与鹰翼具有相同调节能力的翼型或叶片。
Resilient calculating method of bending forming die for wing blade is put forward.
提出了机翼形叶片弯曲成型模的回弹计算方法。
Finally, some specific problems of resilient calculation for wing blade are explained.
最后对机翼形叶片回弹计算的一些具体问题作了说明。
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