A Comprehensive Experimental and Computational Study on LVI induced Damage of Laminated Composites
Author:
Affiliation:
1. University of Michigan, Ann Arbor
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Reference22 articles.
1. Predicting the low velocity impact damage of a quasi-isotropic laminate using EST
2. Low velocity impact modelling in laminate composite panels with discrete interface elements
3. A progressive failure model for composite laminates subjected to low velocity impact damage
4. Low-velocity impact damage on dispersed stacking sequence laminates. Part II: Numerical simulations
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