AA-SM-101-002 Laminate Principal Strain Calculation

October 14, 2014 3:16 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.

General Method

Derives the principle strains in a laminate element given the ABD laminate properties and the input loads.

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