In this module you select core materials from a library or input your own. The length, width and core thickness for the sandwich are first defined. You may now choose from two options. Sandwich buckling lets you select from five different boundary conditions for calculating the minimum uniaxial compression stress for buckling. The bending option determines the maximum deflection due to a uniform distributed load on a simply supported sandwich. Both options calculate face wrinkling and dimpling stresses. MIL-HDBK 23 theory & methods are employed.
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Since 1996 CompositeProTM has been the industry leader, offering tools to help you meet your composite design & analysis challenges. When charts and tables just aren’t enough, and finite element analysis is too much, CompositeProTM fills the void... more
