AA-SM-101-006 Laminate Strain Analysis – Envelope and MS – Compact

October 14, 2014 3:21 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.

Develops a laminate bi-axial strain envelope based on CAI and OHT laminate strain allowables, plots the principal strains on the envelope and calculates the margin of safety. This compact version does not display the envelope graph.

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