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Simulation of Multigeometry Scattering Problems and the Radiation and Refraction of Acoustic Waves through a Shear Layer with Instability Waves SuppressedThe scattering of harmonic acoustic waves at multiple rigid cylinders is simulated applying a Chimera technique and a body-fitted grid approach. The Chimera technique uses a Cartesian background mesh in conjunction with body-fitted O-grids in the immediate vicinity of the solid surfaces to resolve the geometry. The body-fitted grid approach applies a multiblock topology with O-grids wrapping the cylinders while an H-type topology is used away from the cylinders that converges against a Cartesian mesh in the far field. Both grid approaches are compared using a similar far-field resolution of about seven points per wavelength. The refraction of acoustic waves in an unstable jet is simulated using a modification of the linearized Euler equations that can be proven to be stable for arbitrary mean flow fields. The simulations confirm the modified perturbation equations to suppress the excitation of unstable modes. The wave operator encoded in the perturbation equations is known to be exact for irrotational mean flows, that is, in the high-frequency limit of the Strouhal number based on frequency f and mean-flow vorticity ω0 tending to infinity. It is shown that even for a Strouhal numbers of O(1), the modified acoustic perturbation equations resolve mean flow refraction and scattering effects accurately. For the jet, larger differences to the reference solution appear, in particular, downstream of the harmonic source position due to the small Strouhal number in the jet shear layer.
Document ID
20040182283
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
R Ewert
(Deutsche Forschungsanstalt fuer Luft- und Raumfahrt Brunswick Germany)
J Yin
(Deutsche Forschungsanstalt fuer Luft- und Raumfahrt Brunswick, Germany)
J W Delfs
(Deutsche Forschungsanstalt fuer Luft- und Raumfahrt Brunswick Germany)
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
Acoustics
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
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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