Refined design curves for compressive buckling of curved panels using nonlinear finite element analysis
Author:
Affiliation:
1. Bombardier Aerospace, Downsview, Canada
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1328
Reference23 articles.
1. 4Nemeth, M. P. and Starnes Jr., J. H. "The NASA Monographs on Shell Stability Design Recommendations -AReview and Suggested Improvements",NASA TP-1998-206290,January 1998.
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