Buckling analysis of geometrically imperfect stiffened cylinders under axial compression
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.7331
Reference24 articles.
1. 2Deiwert, G. S. "Computation of Separated Transonic Turbulent Flows,"/17/1/I Journal, Vol.14, June 1976, pp.735-740.
2. The Hot-Wire Anemometer in Supersonic Flow
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