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Control of Flow Separation in Adverse Pressure Gradients by Means of Crosswire Grooved Surfaces for Turbo Machine Applications.

Hage, W. and Meyer, R. and Paschereit, C. O. (2008) Control of Flow Separation in Adverse Pressure Gradients by Means of Crosswire Grooved Surfaces for Turbo Machine Applications. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 96. Springer.

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Item URL in elib:https://elib.dlr.de/57708/
Document Type:Article
Title:Control of Flow Separation in Adverse Pressure Gradients by Means of Crosswire Grooved Surfaces for Turbo Machine Applications.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hage, W.UNSPECIFIEDUNSPECIFIED
Meyer, R.UNSPECIFIEDUNSPECIFIED
Paschereit, C. O.Institut für Strömungsmechanik und Technische Akustik, TU BerlinUNSPECIFIED
Date:2008
Journal or Publication Title:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol. 96
Editors:
EditorsEmail
Tropea, C.UNSPECIFIED
Jakirlic, S.UNSPECIFIED
Heinemann, H.-J.UNSPECIFIED
Henke, R.UNSPECIFIED
Hönlinger, H.UNSPECIFIED
Publisher:Springer
Status:Published
Keywords:Flow Separation, Crosswire Grooved Surfaces, Turbo Machines Applications, Fluid Mechanics
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Quiet Air Traffic (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Kaur, Balbir
Deposited On:26 Jan 2009
Last Modified:27 Apr 2009 15:46

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