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Numerical Study on Propagation and Scattering of Sound by Two CylindersThe propagation and scattering of sound by two rigid circular cylinders generated by a spatially distributed axisymmetric periodic acoustic source in the still air are simulated numerically using high-order compact spatial approximation of finite differences and high-order Runge-Kutta time integration. To solve the linearized Euler equations describing the wave propagation, the bipolar curvilinear coordinate system has been used in conservative and non-conservative variants. For bipolar curvilinear coordinate system, lines of the grid coincide with cylinders' envelopes for both cylinders. Use of bipolar coordinate system allows to solve the problem in frame of a single block finite difference methodology. The details of implementation of artificial boundary conditions are discussed for this transformation of coordinates. This study shows numerical robustness and long-time stability of high-order finite-difference compact computations in bipolar coordinates. The results on the fine 600x600 grid coincide well with the analytical solution. The main advantages of the proposed approach are a straightforward coordinate transformation of available single-block finite-difference code in Cartesian or polar coordinates and reasonable processor time.
Document ID
20040182270
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Alex Povitsky
(University of Akron Akron, United States)
Tinghui Zheng
(Concordia University Montreal, Canada)
Georgios H Vatistas
(Concordia University Montreal, Canada)
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
Fluid Mechanics And Thermodynamics
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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