Composite Plates Under Concentrated Load on One Edge and Uniform Load on the Opposite Edge
Application: Stress Analysis in Composites
File Name: Composite_Plates_Under_Concentrated_Load
File Extension: pdf
File Size: 714 KB
This paper develops an efficient closed-form analytical approach to evaluate loading on composite panels. It presents excellent correlation to finite element analysis results and demonstrates useful integration with optimization. This approach is pertinent to many composite applications in the aerospace industry.