Experimental and Numerical Analysis of Composite Folded Sandwich Core Structures Under Compression

Author:

Heimbs S.,Middendorf P.,Kilchert S.,Johnson A. F.,Maier M.

Publisher

Springer Science and Business Media LLC

Subject

Ceramics and Composites

Reference18 articles.

1. Rückert, C.: Double skin composite fuselage design—materials & process approaches for test article realisation. In: SAMPE Europe 25th International Conference, Paris, France, 30 March–1 April 2004, pp. 438–443 (2004)

2. Kolesnikov, B.Y., Herbeck, L.: Carbon fiber composite airplane fuselage: concept and analysis. Paper presented at the ILA International Conference, Berlin, Germany, 11–12 May 2004

3. Kolax, M.: Concept and technology: advanced composite fuselage structures. JEC Composites 10, (6/7), 31–33 (2004)

4. Kehrle, R., Kolax, M.: Sandwich structures for advanced next generation fuselage concepts. In: SAMPE Europe Technical Conference, Toulouse, France, 13–14 September 2006, pp. 11–16 (2006)

5. Aktay, L., Johnson, A.F., Holzapfel, M.: Prediction of impact damage on sandwich composite panels. Comput. Mater. Sci. 32, 252–260 (2005)

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