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Radiation And Refraction Of Sound Waves Through a Two-Dimensional Shear LayerThis report presents solutions to Problem 1 of Category 4 in the 4th CAA Workshop on Benchmark Problems. The problem is numerically solved on a clustered orthogonal grid using a high-order optimized upwind Dispersion- Relation-Preserving scheme. The Perfectly-Matched-Layer (PML) boundary condition in unsplit physical variables is applied to ensure minimum numerical reflections. The numerical results by solving the linearized Euler equations are the total solution, being the superposition of the acoustic wave solution and the instability wave solution. In order to get the instability wave solution, a source term of the same excitation frequency is effectively placed upstream of the region of interest. Such a source term produces a stronger instability wave of the same excitation frequency but a weaker acoustic wave in the region of interest and thus the total solution in this region can well approximate a pure instability wave. The acoustic wave solution, which is desired in the problem, is then successfully achieved by subtracting the instability wave solution from the total solution. The benchmark problem is also analytically solved to an accuracy sufficient to evaluate the numerical solutions.
Document ID
20040182289
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Shi Zheng
(Michigan State University East Lansing, United States)
Steve A E Miller
(Michigan State University East Lansing, United States)
Mei Zhuang
(Michigan State University East Lansing, 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
Numerical Analysis
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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