An Efficient Unsteady Aerodynamic and Aeroacoustic Design Framework Using Discrete Adjoint
Author:
Affiliation:
1. Technical University of Kaiserslautern
2. Stanford University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3369
Reference2 articles.
1. On optimum design in fluid mechanics
2. Aerodynamic design via control theory
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