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Numerical Solutions to the Third CAA Workshop Benchmark ProblemsThis paper presents numerical solutions to the problems of propagation of sound waves through a transonic nozzle, shock-sound interactions, and automobile noise involving feedback of the third NASA Computational Aeroacoustics (CAA) Workshop on benchmark problems. The numerical algorithm is based on a dual time scheme for temporal discretization and a third-order finite volume scheme for spatial discretization. The aims of this study are to apply a dual time stepping scheme to treat aeroacoustic problems of sound propagation and to validate our CAA solver with the benchmark problems for developing a numerical tool for noise analysis and control.
Document ID
Document Type
Conference Paper
Loh, Roy H.
(Boeing Co. Canoga Park, CA United States)
Lin, Wen H.
(Boeing Co. Canoga Park, CA United States)
Date Acquired
August 20, 2013
Publication Date
August 1, 2000
Publication Information
Publication: Third Computational Aeroacoustics (CAA) Workshop on Benchmark Problems
Subject Category
Distribution Limits
Work of the US Gov. Public Use Permitted.
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