Further Study of Unidirectional and Bidirectional Composites under Cylindrical Bending.
Abstract
The results of elasticity solutions for the response of unidirectional and bidirectional laminates are presented in detail and compared to corresponding results given by classical lamination theory. Laminates under uniformly distributed and concentrated loadings are treated. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1971
- Accession Number
- AD0736783
Entities
People
- A. S. D. Wang
- N. J. Pagano
Organizations
- Air Force Research Laboratory