Computational Modeling of Flutter Constraint for High-Fidelity Aerostructural Optimization
Author:
Affiliation:
1. University of Michigan, Ann Arbor
2. Georgia Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-2354
Reference47 articles.
1. A Scalable Parallel Approach for High-Fidelity Aerostructural Analysis and Optimization
2. Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration
3. Buffet-Onset Constraint Formulation for Aerodynamic Shape Optimization
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