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Acoustic Scattering from Multiple Circular Cylinders: Category 2, Problems 1 and 2, Analytic SolutionThe main goal of this benchmark problem set is to assess the ability of computational algorithms to simulate the aeroacoustic phenomenon of linear scattering with increasingly complex geometries. These algorithms may include advanced high-order methods being extended to handle complex grid topologies, or mature structured and unstructured approaches developed for intricate geometries that are either low-order or are being adapted to incorporate high-order algorithms. For the problems considered here, the complex geometry does not arise from the shape of the bodies, which are simple circular cylinders, but by the presence of multiple bodies in the computational domain. This problem also provides a test of numerical robustness, long-time stability, and suitability of far-field radiation boundary conditions for more realistic problems. The solution presented here is discussed in more detail in Ref. 1, which is an extension of the single-scattering solution of Ref. 2. These references should be consulted for more detail on the solution methodology.
Document ID
20040182264
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Scott E Sherer
(United States Air Force Research Laboratory Wright-Patterson AFB, United States)
Date Acquired
August 22, 2013
Publication Date
September 1, 2004
Publication Information
Publication: Fourth Computational Aeroacoustics (CAA): Workshop on Benchmark Problems
Publisher: National Aeronautics and Space Administration
Subject Category
Aerodynamics
Report/Patent Number
NASA/CP-2004-212954
Meeting Information
Meeting: 4th Computational Aeroacoustics (CAA) Workshop on Benchmark Problems
Location: Brook Park, OH
Country: US
Start Date: October 20, 2003
End Date: October 22, 2003
Sponsors: Ohio Aerospace Institute, Glenn Research Center
Funding Number(s)
WBS: 22-781-30-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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