|
|
||
|
|
|
|
DLR, Institute of Composite Structures and Adaptive Systems, Braunschweig Germany
Selected Publications:
B. M. Geier, H. Klein, and R. Zimmermann, “Buckling tests with axially compressed unstiffened cylindrical shells made from CFRP,” in Proceedings, international colloquium on buckling of shell structures, on land, in the sea and in the air, London and New York: Elsevier Applied Sciences, 1991, pp. 498–507.
B. Geier, H. Klein and R. Zimmermann, “Experiments on buckling of CFRP cylindrical shells under non-uniform
axial load,” Proceedings, Int. Conference on Composite Engineering, ICCE71, pp. 28-31, August 1994.
H. Klein, B. Geier, H. C. Goetting, et.al. Buckling testing with curved, stiffened CFRP panels damaged by impact. Proc. Conference on Spacecraft Structures Materials and Mechanical Testing, ESA/CNES/DARA SP-386. June 1996.
Geier, B., Klein, H. and Zimmermann, R. (1997) Buckling tests at DLR, BRITE-EURAM Project BE-7550 “DEVILS”, DLR Report WPO4.OK/DLR (1,2,3), DLR, Braunschweig, Germany.
R. Degenhardt, H. Klein, A. Kling, H. Temmen, R. Zimmermann, “Buckling and postbuckling analysis of shells under quasi-static and dynamic loads”, undated pdf file; no publisher, no references; possibly created about 2001.
R. Degenhardt, H. Klein, H. Temmen, R. Zimmermann, Buckling and postbuckling analysis of shells under quasistatic and dynamic loads, DLR Report, (2002).
R. Rolfes, C. Hühne, A. Kling, H. Temmen, B. Geier, H. Klein, J. Tessmer, R. Zimmermann, “Advances in computational stability analysis of thin-walled aerospace structures regarding postbuckling, robust design and dynamic loading”, in Thin-Walled Structures: Advances in Research, Design and Manufacturing ... edited by J. Loughlan, Fourth International Conference on Thin-Walled Structures, 2004, IOP Publishing Ltd.
Kling A., Degenhardt R., Klein H., Tessmer J., Zimmermann R., “Novel stability design scenario for aircraft structures – simulation and experimental validation”, Proceedings of the 5th International Conference on Computation of Shell and Spatial Structures, 1-4 June, 2005 Salzburg, Austria
R. Zimmermann, H. Klein, and A. Kling, “Buckling and postbuckling of stringer stiffened fibre composite curved panels: tests and computations”, Compos. Struct. 73:2 (2006), 150–161.
R. Degenhardt, A. Kling, H. Klein, W. Hillger, H. C. Goetting, R. Zimmermann and K. Rohwer, “Experiments on buckling and postbuckling of thin-walled CFRP structures using advanced measurement systems,” International Journal of Structural Stability and Dynamics, vol. 7, no. 2, pp. 337-358, 2007.
R. Degenhardt, A. Bethge, A. Kling, R. Zimmermann, K. Rohwer, H. Klein, J. Tessmer, A. Calvi, Probabilistic approach for improved buckling knock-down factors of CFRP cylindrical shells, 1st CEAS European Air and Space Conference, Berlin 2007, CD ISSN 0700-408, pp. 3091-3100.
R. Degenhardt, A. Bethge, A. Kling, R. Zimmermann, K. Rohwer, H. Klein, J. Tessmer, and A. Calvi, “Probabilistic approach for improved buckling knock-down factors of CFRP cylindrical shells,” 2008.
Page 166 / 404