Compression-After-Impact of Sandwich Composite Structures: Experiments and Simulation

Author:

Hasseldine Benjamin,Zehnder Alan,Singh Abhendra,Davidson Barry,Van Hout Ward,Keating Bryan

Publisher

Springer International Publishing

Reference10 articles.

1. Kassapoglou C, Jonas P, Abott R (1988) Compressive strength of composite sandwich panels after impact damage: an experimental and analytical study. J Compos Technol Res 10(2):65–73

2. Tomblin J, Lacy T, Smith B, Hooper S, Vizzini A, Lee S (1999) Review of damage tolerance for composite sandwich airframe structures. Federal Aviation Administration Report No. DOT/FAA/AR-99/49. Office of Aviation Research, U.S. Federal Aviation Administration, Washington, DC

3. Moody RC, Vizzini AJ (2000) Damage tolerance of composite sandwich structures. Federal Aviation Administration Report No. DOT/FAA/AR-99/91. Office of Aviation Research, U.S. Federal Aviation Administration, Washington, DC

4. Hasseldine B, Zehnder A, Keating B, Singh A, Davidson B (2013) Compression after impact of thick sandwich composite structures. In: Proceedings of the 54th AIAA structures, structural dynamics, and materials conference

5. Post D, Han B, Ifju P (2000) Moiré methods for engineering and science - moiré interferometry and shadow moiré. In: Photomechanics. Springer, Berlin, pp 151–196

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