Assumed Stress Finite Element Analysis of Through-Cracks in Angle-Ply Laminates
- 1 September 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (9) , 1125-1132
- https://doi.org/10.2514/3.50862
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Traction Boundary Conditions in Hybrid-Stress Finite-Element ModelAIAA Journal, 1978
- A multilayer hybrid-stress finite element analysis of a through-thickness edge crack in A ± 45° laminateEngineering Fracture Mechanics, 1977
- Finite Element Solutions for Laminated Thick PlatesJournal of Composite Materials, 1972
- Finite Element Methods in Continuum MechanicsPublished by Elsevier ,1972
- Exact Solutions for Rectangular Bidirectional Composites and Sandwich PlatesJournal of Composite Materials, 1970
- Derivation of element stiffness matrices by assumed stress distributionsAIAA Journal, 1964