Influence of geometric nonlinearities on skin-stiffener interface stresses
Author:
Affiliation:
1. Hercules Aerospace Company, Inc., Magna, Utah 84044
2. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11027
Reference11 articles.
1. Postbuckling behavior of selected curved stiffened graphite-epoxy panels loaded in axial compression
2. Calculation of stresses and forces between the skin and stiffener incomposite panels
3. Calculation of stresses in stiffened composite panels
4. Stiffener-skin interactions in pressure-loaded composite panels
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