Hybrid Framework for Reliability-Based Design Optimization of Imperfect Stiffened Shells
Author:
Affiliation:
1. Department of Engineering Mechanics, Dalian University of Technology, 116023 Dalian, People’s Republic of China
2. Department of Structural Design, Beijing Institute of Astronautical Systems Engineering, 100076 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053816
Reference55 articles.
1. Theory of Shell Structures
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5. Buckling load analysis of grid stiffened composite cylinders
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