CFD Method for Aero-acoustics using All-speed Numerical Flux and Preconditioned Implicit Time Integration-Reference-Cited by-同舟云学术

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CFD Method for Aero-acoustics using All-speed Numerical Flux and Preconditioned Implicit Time Integration

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:20th AIAA Computational Fluid Dynamics Conference
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Author:

Shima Eiji¹,Kitamura Keiichi¹

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3045

Reference12 articles.

1. E.ShimaandK.Kitamura,"OnNewSimpleLow-DissipationSchemeofAUSM-FamilyforAllSpeeds",AIAA-Paper2009-136,2009

2. E.ShimaandK.Kitamura,"OnAUSM-FamilySchemeforAllSpeedswithShockDetectionforCarbuncle-Fix",AIAA-Paper2009-3544,2009

3. E.Turkel,"Preconditionedmethodsforsolvingtheincompressibleandlowspeedcompressibleequations",J.Comp.Phys.,Vol72,Issue2,(1987)

4. J.M.WeissandW.A.Smith,PreconditioningAppliedtoVariableandConstantDensityFlows,AIAAJ.,Vol.33,No.11,pp.2050-2057(1995)

5. D.UnrauandD.W.Zingg,"ViscousAirfoilComputationsusingLocalPreconditioning,AIAAPaper90-2027(1997)

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