This is a follow on to the previous post of the FPL reports here.
We have taken the derivation for the sandwich compression panel buckling coefficient and made it available in spreadsheet form. We have also started to upload our general set of sandwich analysis spreadsheets.
These spreadsheets are numbered AA-SM-102-XXX and include
AA-SM-102-001 – Composites – Cored Laminate Basic Stiffness Properties
AA-SM-102-003 – Composites – Determination of KM for Cored Panel Compression Buckling
AA-SM-102-010 – Composites – Cored Panel Shear Crimping
AA-SM-102-011 – Composites – Cored Panel Intracellular Buckling
AA-SM-102-012 – Composites – Cored Panel Facesheet Wrinkling
Lots more to come, including shear buckling of sandwich panels and the strength of inserts in sandwich panels.
To try our free Stress Analysis Engineering Spreadsheets click below
To try our Add-in for Microsoft Excel for Windows click below
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