Composite Interaction Energy and Constituent Average Stresses for Predicting Composite Failure
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Wyoming, Laramie, Wyoming 82071
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052890
Reference27 articles.
1. A comparison of the predictive capabilities of current failure theories for composite laminates, judged against experimental evidence
2. A further assessment of the predictive capabilities of current failure theories for composite laminates: comparison with experimental evidence
3. Maturity of 3D failure criteria for fibre-reinforced composites: Comparison between theories and experiments: Part B of WWFE-II
4. Application of progressive fracture analysis for predicting failure envelopes and stress–strain behaviors of composite laminates: a comparison with experimental results
5. Prediction of composite laminate fracture: micromechanics and progressive fracture
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