A numerical and experimental study of the response of selected compression-loaded composite shells with cutouts
Author:
Affiliation:
1. Michigan, Univ., Ann Arbor
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1988
Reference14 articles.
1. 2Lekerkerker, J. G. "On the Stress Distribution in Cylindrical Shells Weakened by a Circular Hole," Ph.D. dissertation,Technological University, Delft, TheNetherlands,1965.
2. Buckling of cylinders with cutouts
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