Analytical-Experimental Correlation for a Stiffened Composite Panel Loaded in Axial Compression
Author:
Affiliation:
1. University of Florida, Gainesville, Florida 32611-6250
2. NASA Langley Research Center, Hampton, Virginia 23681
3. General Electric Corporate Research & Development Center, Schenectady, New York 1230
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2772
Reference13 articles.
1. PANDA2—Program for minimum weight design of stiffened, composite, locally buckled panels
2. Design of a blade-stiffened composite panel with a hole
3. Buckling and failure characteristics of compression-loaded stiffened composite panels with a hole
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