Unsteady Optimization Using a Discrete Adjoint Approach Applied to Aeroacoustic Shape Design

Author:

Rumpfkeil Markus1,Zingg David1

Affiliation:

1. University of Toronto

Publisher

American Institute of Aeronautics and Astronautics

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. On-the-Fly Unsteady Adjoint Aerodynamic and Aeroacoustic Optimization Method;AIAA Journal;2024-08-13

2. Optimizing Proprotor Blades Using Coupled Aeroacoustic and Aerodynamic Sensitivities;AIAA AVIATION 2021 FORUM;2021-07-28

3. Toward Adjoint-Based Aeroacoustic Optimization for Propeller and Rotorcraft Applications;AIAA AVIATION 2020 FORUM;2020-06-08

4. Sensitivity Analysis of Broadband Shock-Associated Noise based on Navier-Stokes Equations Decomposition;AIAA Scitech 2020 Forum;2020-01-05

5. A Coupled-Adjoint Method for Aerodynamic and Aeroacoustic Optimization;12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2012-09-11

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