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

Hergt, Alexander and Meyer, Robert and Engel, Karl (2013) Effects of Vortex Generator Application on the Performance of a Compressor Cascade. ASME Journal of Turbomachinery, 135 (2), 021027-1. American Society of Mechanical Engineers (ASME). ISSN 0889-504X

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Item URL in elib:https://elib.dlr.de/82665/
Document Type:Article
Title:Effects of Vortex Generator Application on the Performance of a Compressor Cascade
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hergt, Alexanderalexander.hergt (at) dlr.deUNSPECIFIED
Meyer, Robertrobert.meyer (at) dlr.deUNSPECIFIED
Engel, KarlMTU Aero Engines GmbHUNSPECIFIED
Date:March 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
Volume:135
Page Range:021027-1
Publisher:American Society of Mechanical Engineers (ASME)
ISSN:0889-504X
Status:Published
Keywords:Vortex Generator Application, Secondary Flow, Flow Control Compressor Cascade
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 - Fan and Compressor Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Hergt, Dr.-Ing. Alexander Silvio
Deposited On:20 Jun 2013 09:48
Last Modified:08 Mar 2018 18:53

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