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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. (Submitted)

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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 Authors
Hage, W.UNSPECIFIED
Meyer, R.UNSPECIFIED
Paschereit, C. O.Institut für Strömungsmechanik und Technische Akustik, TU Berlin
Date:2007
Journal or Publication Title:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Refereed publication:Yes
In ISI Web of Science:No
Editors:
EditorsEmail
Tropea, C.UNSPECIFIED
Jakirlic, S.UNSPECIFIED
Heinemann, H.-J.UNSPECIFIED
Henke, R.UNSPECIFIED
Hönlinger, H.UNSPECIFIED
Publisher:Springer
Status:Submitted
Keywords:Turbo Machine Applications, Numerical Fluid Mechanics
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems
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: Balbir Kaur
Deposited On:02 Jul 2007
Last Modified:15 Jan 2010 00:57

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