Stress considerations in reduced-size aeroelastic optimization
Author:
Affiliation:
1. Technion—Israel Institute of Technology, Haifa 32000, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12447
Reference17 articles.
1. Practical Design of Minimum-Weight Aircraft Structures for Strength and Flutter Requirements
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