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
Open source: license | download
View All Supporting Documents
Location of all "Composite Laminate Analysis" Users Since Its Posting