AA-SM-103-001 Composites – Buckling of Foam Core Sandwich Panels – Simple

October 14, 2014 3:53 pm

Sample Engineering Spreadsheets Provided by Abbott Aerospace Inc

This spreadsheet uses the XL-Viking Plugin to display equations. The Spreadsheet will calculate correctly without the plugin and can be used ‘as is’ but none of the math will be visible. To find out more about XL-Viking click here.

References:
Ref Mil-Hndbk-23, Section 5.3

Description:
Shear and compression buckling of a cored sandwich panel with isotropic face sheets.

 


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