Leading edge noise studies using CAA

Author:

Delfs Jan1,Yin Jianping1,Li Xiaodong2

Affiliation:

1. DLR, Braunschweig, Germany

2. Beijing Univ. of Aeronautics and Astronautics, China

Publisher

American Institute of Aeronautics and Astronautics

Cited by 5 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. The Response of a Flat Plate Cascade to Sinusoidal Gusts;37th AIAA Fluid Dynamics Conference and Exhibit;2007-06-15

2. Acoustic perturbation equations based on flow decomposition via source filtering;Journal of Computational Physics;2003-07

3. Sound generation from gust-airfoil interaction using CAA-Chimera method;7th AIAA/CEAS Aeroacoustics Conference and Exhibit;2001-05-28

4. Numerical description of acoustic sources in airframe noise;ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik;2001

5. Aeroacoustic source terms for the linearized Euler equations;6th Aeroacoustics Conference and Exhibit;2000-06-12

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