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Design study of a two-parted variable inlet guide vane with an optimized axial gap

Gouezou, William (2017) Design study of a two-parted variable inlet guide vane with an optimized axial gap. Other, ENSIAME (École nationale supérieure d'ingénieurs en informatique, automatique, mécanique, énergétique et électronique).

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Item URL in elib:https://elib.dlr.de/114831/
Document Type:Thesis (Other)
Title:Design study of a two-parted variable inlet guide vane with an optimized axial gap
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Gouezou, WilliamUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:October 2017
Refereed publication:No
Open Access:Yes
Number of Pages:71
Status:Unpublished
Keywords:compressor, variable inlet guide vane, design optimization
Institution:ENSIAME (École nationale supérieure d'ingénieurs en informatique, automatique, mécanique, énergétique et électronique)
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 (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Pottmann, Stefan
Deposited On:02 Nov 2017 10:41
Last Modified:13 Feb 2026 13:51

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