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Investigation of nonreflective boundary conditions for computational aeroacoustics
2006 (English)In: AIAA Journal, ISSN 0001-1452, E-ISSN 1533-385X, Vol. 44, no 9, 1932-1940 p.Article in journal (Refereed) Published
Abstract [en]

Direct aeroacoustic computations require nonreflective boundary conditions that allow disturbances to leave the domain freely without anomalous reflections. In the present paper we analyze a series of nonreflective boundary conditions already published in the literature and propose an improved outflow nonreflective boundary condition with reflection characteristic that is reduced greatly. For the solution of the linearized Euler equations, a sixth-order compact finite-difference algorithm is used together with a sixth-order explicit digital filter that suppresses the high-frequency spurious oscillations in the solution. A number of representative test cases are presented. The new outflow boundary condition is recommended for the simulation of sound produced by turbulence.

Place, publisher, year, edition, pages
2006. Vol. 44, no 9, 1932-1940 p.
Keyword [en]
perfectly matched layer, aerodynamic sound, simulations, flows
URN: urn:nbn:se:kth:diva-15341DOI: 10.2514/1.5807ISI: 000240413100002OAI: diva2:333382
QC 20100525Available from: 2010-08-05 Created: 2010-08-05 Last updated: 2011-07-07Bibliographically approved

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Fuchs, Laszlo
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