AA-SM-113 Composites – Sandwich Panels Under Pressure

October 14, 2014 5:16 pm

Sample Engineering Spreadsheets Provided by Abbott Aerospace Inc

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References:
NASA Structures Manual TM X-73305, Chapter B9.6 Structural Sandwich Plates, Subchapter B9.6.1.1 Basic Principles for Design of Flat Sandwich Panels under Uniformly Distributed Normal Load.
Bruhn, Para. A17.7, Large Deflections Theory

Description:
Methods for the stress analysis for small and large deflections on sandwich plates.


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