Relevance of 3D simulations and sandwich core topology for the modeling of honeycomb core sandwich panels undergoing interfacial crack propagation

Author:

Höwer Daniel,Jois Kumar C.,Lerch Bradley A.,Bednarcyk Brett A.,Pineda Evan J.,Reese Stefanie,Simon Jaan-Willem

Funder

Excellence Initiative of the German federal and state governments

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference68 articles.

1. Impact damage resistance and tolerance of honeycomb core sandwich panels;Raju;J Compos Mater,2008

2. McQuigg TS, Kapania RK, Scotti SJ, .Walker SP. Compression after impact on honeycomb core sandwich panels with thin facesheets. Part 1: experiments. In: 53rd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference; 2012.

3. Ratcliffe JG, Jackson WC. A finite element analysis for predicting the residual compressive strength of impact-damaged sandwich panels. NASA/TM-2008-215341.

4. Numerical modeling of impact-damaged sandwich composites subjected to compression-after-impact loading;Lacy;Compos Struct,2003

5. Hodge A, Nettles A, Jackson J. Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage, NASA/TP-2011-216460.

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