AA-SM-113 Composites – Sandwich Panels Under Pressure
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.
NASA Structures Manual TM X-73305, Chapter B9.6 Structural Sandwich Plates, Subchapter B188.8.131.52 Basic Principles for Design of Flat Sandwich Panels under Uniformly Distributed Normal Load.
Bruhn, Para. A17.7, Large Deflections Theory
Methods for the stress analysis for small and large deflections on sandwich plates.