Reliability-Based Wing Design Optimization Using Trust Region-Sequential Quadratic Programming Framework
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Daejon 305-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.11978
Reference20 articles.
1. Effect of Random Geometric Uncertainty on the Computational Design of a 3D Flexible Wing
2. Reliability-Based Design Optimization of Aeroelastic Structures
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