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Numerical Validation of Composite Panel Impact Tests

Authors :
Loukham Shamsunder
Bilal Khaled
Subramaniam D. Rajan
J. Michael Pereira
Paul DuBois
Gunther Blankenhorn
Source :
International Journal of Impact Engineering. 159
Publication Year :
2021
Publisher :
United States: NASA Center for Aerospace Information (CASI), 2021.

Abstract

Researchers have met the challenge of modeling impact events involving composite targets for a variety of applications in a variety of ways. In this paper, the theory and implementation details of an orthotropic visco-elastic-visco-plastic material model with strain rate dependence are discussed. The model is driven by experimental data from quasi-static as well as high strain rate tests, and the data is used in defining the deformation, damage and failure sub-models. Validation data is generated by shooting a hollow 50 g Al-2024 projectile at different velocities against a flat panel target made of unidirectional composite material in a 16-ply [(0/90/45/-45)_(2)]_(S) layup. Explicit dynamic finite element analyses of four high speed tests involving one contained (projectile rebounded) and three uncontained (projectile penetrated) impact tests show that the developed material model and modeling techniques yield reasonable and acceptable predictions.

Subjects

Subjects :
Composite Materials

Details

Language :
English
ISSN :
18793509 and 0734743X
Volume :
159
Database :
NASA Technical Reports
Journal :
International Journal of Impact Engineering
Notes :
816088.04.03.02.02, , #12-G-001, , 17-G-005
Publication Type :
Report
Accession number :
edsnas.20210021698
Document Type :
Report
Full Text :
https://doi.org/10.1016/j.ijimpeng.2021.104032