Fracture Analysis of a Curvilinearly Stiffener Panel Subjected to Multiple Combined Loadings
Author:
Affiliation:
1. Engineering Science and Mechanics, 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/10.2514/1.C032071
Reference57 articles.
1. Future of Flight Vehicle Structures (2000 to 2023)
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