Strain-Rates Dependent Constitutive Law for Crashworthiness and Parameter Sensitivity Analysis of Woven Composites

Author:

Lombarkia R.ORCID,Gakwaya A.,Nandlall D.,Dano M. L.,Lévesque J.,Vachon-Joannette P.,Gagnon P.,Benkhelifa A.

Publisher

Springer Science and Business Media LLC

Reference46 articles.

1. Tabiei, A., Medikonda, S.: A non-linear strain-rate micro-mechanical composite material model for impact problems. In: 15th International LS-DYNA Users Conference, Detroit, 10–12 June 2018, pp 1–22 (2018)

2. Palma, L.D., Caprio, F.D., Chiariello, A., Ignarra, M., Russo, S., Riccio, A., Luca, A.D., Caputo, F.: Vertical drop test of composite fuselage section of a regional aircraft. AIAA J. 58(1), 474–487 (2020)

3. Caputo, F., Lamanna, G., Perfetto, D.: Experimental and numerical crashworthiness study of a full-scale composite fuselage section. AIAA J. (2020). https://doi.org/10.2514/1.J059216

4. Fasanella, E.L., Jackson, K.E.: Best practices for crash modeling and simulation. In: Technical Memorandum: NASA/TM-2002-211944, Ref. ARL-TR-2849 (2002)

5. McGregor, C.J.: Simulation of progressive damage development in braided composite tubes under axial compression. Master’s thesis, University of British Columbia, Vancouver (2005)

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