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

Hage, W. and Meyer, R. and Paschereit, C. O. (2007) Control of flow Separation in Adverse Pressure Gradients by Means of Crosswise Grooved Surfaces for Turbo Machine Applications. Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer. doi: 10.1007/978-3-540-74460-3_40. ISBN 978-3-540-74458-0.

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Item URL in elib:https://elib.dlr.de/49131/
Document Type:Article
Title:Control of flow Separation in Adverse Pressure Gradients by Means of Crosswise Grooved Surfaces for Turbo Machine Applications.
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Hage, W.UNSPECIFIEDUNSPECIFIED
Meyer, R.UNSPECIFIEDUNSPECIFIED
Paschereit, C. O.Institut für Strömungsmechanik und Technische Akustik, TU BerlinUNSPECIFIED
Date:2007
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
DOI:10.1007/978-3-540-74460-3_40
Editors:
EditorsEmailEditor's ORCID iD
Tropea, C.UNSPECIFIEDUNSPECIFIED
Jakirlic, S.UNSPECIFIEDUNSPECIFIED
Heinemann, H.-J.UNSPECIFIEDUNSPECIFIED
Henke, R.UNSPECIFIEDUNSPECIFIED
Hönlinger, H.UNSPECIFIEDUNSPECIFIED
Publisher:Springer
ISBN:978-3-540-74458-0
Status:Published
Keywords:Turbo Machine Applications, Numerical Fluid Mechanics
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:L VU - Air Traffic and Environment (old)
DLR - Research area:Aeronautics
DLR - Program:L VU - Air Traffic and Environment
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:02 Jul 2007
Last Modified:28 Jul 2022 12:09

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