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fastADER: An Arbitrary High Order Scheme for Linear AcousticsFor the solution of aeroacoustical problems, it is necessary to use high order schemes to resolve the wave propagation accurately over long distances. Sixth order Finite-Difference schemes are used commonly in space, although the discretization method for time integration is often a fourth order accurate Runge Kutta type integration and thus the overall scheme remain fourth order. The fastADER approach is not suffering from the order restriction of the Runge-Kutta schemes, the so called Butcher barrier. The schemes have uniform, arbitrary order in space and time. The schemes can be implemented highly efficiently if the following conditions are fulfilled: globally linearized hyperbolic PDE's discretized on Cartesian grids. The CPU time grows quadratically with the order while no extra memory is needed. In the paper a von Neumann stability test, amplitude and phase error diagrams as well as numerical convergence rates are included thus giving a good overview of the method.
Document ID
20040182296
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
T Schwartzkopff
(Stuttgart Univ. Stuttgart, Germany)
C-D Munz
(Stuttgart Univ. Stuttgart, 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
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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