Implementing deformation, damage, and failure in an orthotropic plastic material model

Author:

Shyamsunder Loukham1,Khaled Bilal1,Rajan Subramaniam D1ORCID,Goldberg Robert K2,Carney Kelly S3,DuBois Paul3,Blankenhorn Gunther4

Affiliation:

1. School of Sustainable Engineering and the Built Environment, Arizona State University, USA

2. Aerospace Engineer, Structures and Materials Division, NASA Glenn Research Center, USA

3. Research Scientist, George Mason University, USA

4. Software Engineer, LSTC, USA

Abstract

Theoretical and implementation details of an orthotropic plasticity model are presented. The model is comprised of three sub-models dealing with elastic and inelastic deformations, damage, and failure. The input to the three sub-models involves tabulated data that can be obtained from laboratory and/or virtual testing. In this article, the focus is on the development of the failure sub-model and its links to the other components. Details of how the user-selected failure criterion is used, and what steps are implemented post-failure are presented. The well-known Puck failure criterion is used in the numerical examples. Three validation tests are used to illustrate the strengths and weaknesses of the failure sub-model—10°, 15°, and 30° off-axis tests, a stacked-ply test carried out at room temperature under quasi-static loading, and finally, a high-speed impact test. Results indicate that while the deformation and damage sub-models give reasonably accurate results, the failure predictions are a huge challenge especially for high-speed impact tests.

Funder

National Aeronautics and Space Administration

Federal Aviation Administration

Publisher

SAGE Publications

Subject

Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

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