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Author Topic: how to realize wing tip optimization ?  (Read 15188 times)


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how to realize wing tip optimization ?
« on: July 28, 2009, 01:48:29 AM »

how to  realize wing tip optimization ? I mean to optimize the global stiffness of wing by limiting wing tip deflection and twist, and to make the wing spanwise distortion smooth.

by using Object Model? if how?

I know wing tip displacement limits can be given when running hyperFEA, but I am not sure whether the spanwise distortion is smooth.