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Effects of Vortex Generator Application on the Performance of a Compressor Cascade

Hergt, A. and Meyer, R. and Engel, K. (2010) Effects of Vortex Generator Application on the Performance of a Compressor Cascade. In: Proceedings of the ASME TURBO EXPO (Paper GT2010-22464). ASME Turbo Expo 2010: Power for Land, Sea and Air, 14.-18. Juni 2010, Glasgow, United Kingdom. ISBN 9780791838723.

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Document Type:Conference or Workshop Item (Paper)
Title:Effects of Vortex Generator Application on the Performance of a Compressor Cascade
Authors:
AuthorsInstitution or Email of Authors
Hergt, A.UNSPECIFIED
Meyer, R.UNSPECIFIED
Engel, K.MTU Aero Engines GmbH, München
Date:2010
Journal or Publication Title:Proceedings of the ASME TURBO EXPO
Refereed publication:Yes
In ISI Web of Science:No
ISBN:9780791838723
Status:Published
Keywords:Vortex Generator, Compressor Cascade
Event Title:ASME Turbo Expo 2010: Power for Land, Sea and Air
Event Location:Glasgow, United Kingdom
Event Type:international Conference
Event Dates:14.-18. Juni 2010
Organizer:ASME
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Turbine Technologies
Location: Köln-Porz , Berlin-Adlershof
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Institute of Propulsion Technology > Fan and Compressor
Deposited By: Balbir Kaur
Deposited On:01 Feb 2011 10:04
Last Modified:01 Feb 2011 10:11

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