Integrated Global Wing and Local Panel Optimization of Aircraft Wing
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0137
Reference36 articles.
1. MultiLevel Approach to Minimum Weight Deesign Including Buckling Constraints
2. Structural synthesis - Its genesis and development
3. Comparison of Two Types of Structural Optimization Procedures for Flutter Requirements
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