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Author Topic: Buckling - Panels with holes (Orthotropic and Isotropic Materials)  (Read 19280 times)

Stressed

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Buckling - Panels with holes (Orthotropic and Isotropic Materials)
« on: July 31, 2009, 09:43:47 AM »
A suggestion for a future upgrade

A large number of panels in wing spars, ribs and skin have access or lightening holes. Hypersizer should have the capability to calculate the buckling allowable for a panel with a circular hole. More complex configurations would require a detailed FEM.
« Last Edit: July 31, 2009, 09:46:48 AM by Stressed »
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David Johnson
Hitech Global Solutions Inc
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