Find information on common issues.
Ask questions and find answers from other users.
Suggest a new site feature or improvement.
Check on status of your tickets.
By Andrew Ritchey
Uses basic laminate theory to estimate effective laminate properties and residual stresses, strains and deformations due to thermal loading.
You must login before you can run this tool.
Version 1.2x - published on 22 Apr 2016
doi:10.4231/D33X83M8K cite this
View All Supporting Documents