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Design Study of a Two-Parted Variable Inlet Guide Vane with an Optimized Axial Gap

Gouezou, William and Hemmert-Pottmann, Stefan and Nicke, Eberhard (2017) Design Study of a Two-Parted Variable Inlet Guide Vane with an Optimized Axial Gap. Deutscher Luft- und Raumfahrtkongress, 05-07 Sep 2017, Munich, Germany.

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Item URL in elib:https://elib.dlr.de/115570/
Document Type:Conference or Workshop Item (Lecture)
Title:Design Study of a Two-Parted Variable Inlet Guide Vane with an Optimized Axial Gap
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gouezou, Williamwilliam.gouezou (at) dlr.deUNSPECIFIED
Hemmert-Pottmann, Stefanstefan.hemmert-pottmann (at) dlr.dehttps://orcid.org/0000-0003-1397-750X
Nicke, Eberhardeberhard.nicke (at) dlr.deUNSPECIFIED
Date:7 September 2017
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:axial compressor, design optimization, variable inlet guide vane
Event Title:Deutscher Luft- und Raumfahrtkongress
Event Location:Munich, Germany
Event Type:national Conference
Event Dates:05-07 Sep 2017
Organizer:Deutsche Gesellschaft für Luft- und Raumfahrt
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:propulsion systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Fan and Compressor Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Hemmert-Pottmann, Stefan
Deposited On:21 Nov 2017 10:08
Last Modified:21 Nov 2017 10:08

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