Leading edge noise studies using CAA
Author:
Affiliation:
1. DLR, Braunschweig, Germany
2. Beijing Univ. of Aeronautics and Astronautics, China
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1897
Reference12 articles.
1. Dispersion-Relation-Preserving Finite Difference Schemes for Computational Acoustics
2. 4Khorrami, M.R.; Singer, B.A."Stability Analysis for Noise-Source Modeling of a Part-Span flap0022, AIAA Paper 9% 2225, 1998.
3. onkewitz, P.; Huerre, P.; Chomaz, J. "Global linear stability analysis of weakly non-parallel shear flows0022, J.Fluid Mech., Vol.251, pp. l-20, 1993.
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