Some Approximation Concepts for Structural Synthesis
Author:
Affiliation:
1. University of California, Los Angeles, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49321
Reference19 articles.
1. Minimum-weight stiffened shells with slight meridional curvature designed to support axial compressive loads.
2. A Mixed Optimization Method for Automated Design of Fuselage Structures
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