Optimal design of ring stiffened cylindrical shells using multiple stiffener sizes
Author:
Affiliation:
1. New Jersey Institute of Technology, Newark, N.J.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.7707
Reference6 articles.
1. Minimum weight design of cylindrical shell with multiple stiffener sizes
2. Extended capability for automated design of frame-stiffened, submersible, cylindrical shells
3. Response of oddly-stiffened circular cylindrical shells
4. A Boundary Tracking Optimization Algorithm for Constrained Nonlinear Problems
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3. Optimal design of imperfect, anisotropic, ring-stiffened cylinders under combined loads;Structural Optimization;1995-07
4. OPTIMAL DESIGN OF IMPERFECT, ANISOTROPIC, RING-STIFFENED CYLINDERS UNDER COMBINED LOADS;34th Structures, Structural Dynamics and Materials Conference;1993-04-19
5. Shells;Optimal Structural Design under Stability Constraints;1988
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