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Advanced Numerical Methods For The Prediction Of Tonal Noise In Turbomachinery, Part I: Implicit Runge-Kutta Schemes

Ashcroft, Graham and Frey, Christian and Heitkamp, Kathrin and Weckmüller, Christian (2013) Advanced Numerical Methods For The Prediction Of Tonal Noise In Turbomachinery, Part I: Implicit Runge-Kutta Schemes. ASME Journal of Turbomachinery (136). American Society of Mechanical Engineers (ASME). DOI: 10.1115/1.4023904 ISSN 0889-504X

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Official URL: http://turbomachinery.asmedigitalcollection.asme.org/article.aspx?articleID=1744977


Item URL in elib:https://elib.dlr.de/87883/
Document Type:Article
Title:Advanced Numerical Methods For The Prediction Of Tonal Noise In Turbomachinery, Part I: Implicit Runge-Kutta Schemes
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Ashcroft, Grahamgraham.ashcroft (at) dlr.deUNSPECIFIED
Frey, ChristianChristian.Frey (at) dlr.deUNSPECIFIED
Heitkamp, Kathrinkathrin.heitkamp (at) dlr.deUNSPECIFIED
Weckmüller, ChristianChristian.Weckmueller (at) dlr.deUNSPECIFIED
Date:2013
Journal or Publication Title:ASME Journal of Turbomachinery
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI :10.1115/1.4023904
Publisher:American Society of Mechanical Engineers (ASME)
ISSN:0889-504X
Status:Published
Keywords:Turbomachinery Noise, Implicit Runge-Kutta
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Virtual Engine and Validation Methods (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Institute of Propulsion Technology > Numerical Methodes
Institute of Propulsion Technology > Engine Acoustic
Deposited By: Ashcroft, Dr.(PH.D.) Graham
Deposited On:10 Feb 2014 09:00
Last Modified:08 Mar 2018 18:53

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