Efficient Airframe Noise Reduction Framework via Adjoint-Based Shape Optimization
Author:
Affiliation:
1. University of Kaiserslautern, 67663 Kaiserslautern, Germany
2. Embraer S.A., São José dos Campos 12277-901, Brazil
3. Bosch Research and Technology Center, Sunnyvale, 94085 CA
4. Stanford University, Stanford, 94305 CA
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference43 articles.
1. LockardD. P.LilleyG. M. “The Airframe Noise Reduction Challenge,” NASA TM-2004-213013, 2004.
2. Aerodynamic design via control theory
3. On optimum design in fluid mechanics
4. A hybrid algorithm for far-field noise minimization
5. A Coupled-Adjoint Method for Aerodynamic and Aeroacoustic Optimization
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