Investigation of Buckling Behavior of Composite Shell Structures with Cutouts

Author:

Arbelo Mariano A.,Herrmann Annemarie,Castro Saullo G. P.,Khakimova Regina,Zimmermann Rolf,Degenhardt Richard

Publisher

Springer Science and Business Media LLC

Subject

Ceramics and Composites

Reference21 articles.

1. Agency, E.S.: SA Studies future of Europe’s launch services. 25 July 2012. [Online]. Available: http://www.esa.int/Our_Activities/Launchers/ESA_studies_future_of_Europe_s_launch_services . [Accessed 12 March 2013]

2. Koiter, W.T.: A translation of the stability of elastic equilibrium. Technische Hooge School at Delft, Department of Mechanics, Shipbuilding and Airplane Building. 14th November. (1945)

3. Weingarten, V.I., Seide, P., and Peterson, J.P.: NASA SP-8007 - buckling of thin-walled circular cylinders. NASA Space Vehicle Design Criteria - Structures, 1965 (revised 1968)

4. Nemeth, M.P., Starnes, J.A.J.: The NASA monographs on shell stability design recommendations, NASA/TP-1998-206290. National Aeronautics and Space Administration, Langley Research Center, p. 20 (1998)

5. Tennyson, R.C.: The effect of unreinforced circular cutouts on the buckling of circular cylindrical shells under axial compression. J. Eng. Ind., 541–546 (1968)

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