Towards adjoint-based methods for aeroacoustic control-Reference-Cited by-同舟云学术

Towards adjoint-based methods for aeroacoustic control

Published:2001-01-08 Issue: Volume: Page:
ISSN:
Container-title:39th Aerospace Sciences Meeting and Exhibit
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Author:

Collis S.¹,Ghayour Kaveh¹,Heinkenschloss Matthias¹,Ulbrich Michael²,Ulbrich Stefan²

Affiliation:

1. Rice Univ., Houston, TX

2. Muenchen, Technische Univ., Munich, Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-821

Reference31 articles.

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2. 3Wang, B.,Baeder,J. D.,and Singh, R.K."AComputational Study ofTrailing-Edge FlapAerodynamics and Acoustics,"55thAnnualForum of theAmerican Helicopter Society, May 1999.

3. 4Collis, S.S.and Lele, S.K."A Computational Investigation of Receptivity in High-Speed Flow Near a Swept Leading-Edge," Tech. Rep. TF-71, Flow Physics andComputation Division, Department of Mechanical Engineering, Stanford University, April 1997.

4. Numerical Solution of a Flow-Control Problem: Vorticity Reduction by Dynamic Boundary Action

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