Failure Model for Rate-Dependent Polymer Matrix Composite Laminates under High-Velocity Impact

Author:

Zhu Linfa123,Chattopadhyay Aditi123,Goldberg Robert K.123

Affiliation:

1. Software Engineer, Altair Engineering, Inc., Austin, TX 78757.

2. Professor, Dept. of Mechanical and Aerospace Engineering, Arizona State Univ., Tempe, AZ 85287.

3. Aerospace Engineer, Mechanics and Life Prediction Branch, NASA Gleen Research Center, Cleveland, OH 44135.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference18 articles.

1. A Progressive Damage Model for Laminated Composites Containing Stress Concentrations

2. High velocity impact of thick composites

3. Dey S. (2004). “High-strength steel plates subjected to projectile impact—An experimental and numerical study.” Doctoral dissertation Norwegian Univ. of Science and Technology Trondheim Norway.

4. Goldberg R. K. Roberts G. D. and Gilat A. (2003). “Implementation of an associative flow rule including hydrostatic stress effects into the high strain rate deformation analysis of polymer matrix composites.” NASA/TM-2003-212382 NASA Washington D.C.

5. Failure Criteria for Unidirectional Fiber Composites

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