A Coupled-Adjoint Method for Aerodynamic and Aeroacoustic Optimization
Author:
Affiliation:
1. Stanford University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-5598
Reference15 articles.
1. Aerodynamic shape optimization techniques based on control theory
2. Aerodynamic design via control theory
3. Optimum Shape Design for Unsteady Flows with Time-Accurate Continuous and Discrete Adjoint Method
4. Discrete Adjoint-Based Design for Unsteady Turbulent Flows on Dynamic Overset Unstructured Grids
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