Framework for Multifidelity Aeroelastic Vehicle Design Optimization
Author:
Affiliation:
1. University of Dayton
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4322
Reference26 articles.
1. Identification of Critical Flight Loads
2. A trust region framework for managing approximation models in engineering optimization
3. A Design Study Employing Aeroelastic Tailoring and an Active Aeroelastic Wing Design Approach on a Tailless Lambda Wing Configuration
4. An adaptive approach to constraint aggregation using adjoint sensitivity analysis
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