Comparison of Test Methods to Determine Failure Parameters for MAT162 Calibration
Author:
Affiliation:
1. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1701
Reference14 articles.
1. Progressive Damage and Failure Prediction of Open Hole Tension and Open Hole Compression Specimens
2. Comparison of composite damage growth tools for static behavior of notched composite laminates
3. Prediction of Low-Velocity Face-on Impact Response of Composite Laminates using High-Fidelity Finite Element Modeling Techniques
4. Face-on and Edge-on Impact Response of Composite Laminates
5. NASA ACC High Energy Dynamic Impact Methodology and Outcomes
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2. The Use of Depth of Penetration Testing to Develop Element Erosion Parameters in LS-DYNA Explicit Simulations;AIAA Scitech 2019 Forum;2019-01-06
3. Verification Benchmarks and Validation of Advanced Features of MAT261 for High Energy Dynamic Impact Applications;AIAA Scitech 2019 Forum;2019-01-06
4. NASA ACC High Energy Dynamic Impact Methodology and Outcomes;2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2018-01-07
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