Ewert, R. and Yin, J. and Delfs, J. (2003) Simulation of Multi-Geometry Scattering Problems and the Radiation and Refraction of Acoustic Waves Through a Shear Layer with Instability Waves Suppressed. 4th Computational Aeroacoustics (CAA) Workshop on Benchmark Problems, Brook Park/Cleveland (usa), 08.-10.10.2003.
Full text not available from this repository.
The 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. 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 Type:||Conference or Workshop Item (Paper)|
|Title:||Simulation of Multi-Geometry Scattering Problems and the Radiation and Refraction of Acoustic Waves Through a Shear Layer with Instability Waves Suppressed|
|Keywords:||CAA, CAA-Chimera, a body-fitted grid, linearized Euler equations, multiple rigid cylinder, Acoustic Scattering|
|Event Title:||4th Computational Aeroacoustics (CAA) Workshop on Benchmark Problems, Brook Park/Cleveland (usa), 08.-10.10.2003|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - The Quiet and Comfortable Rotorcraft|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology|
|Deposited By:||Claudia Grant|
|Deposited On:||31 Jan 2006|
|Last Modified:||14 Jan 2010 19:54|
Repository Staff Only: item control page