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Optimised Aerodynamic Design of An OGV With Reduced Blade Count For Low Noise Aircraft Engines

Kröger, Georg and Schnell, Rainer and Humphreys, Nick (2012) Optimised Aerodynamic Design of An OGV With Reduced Blade Count For Low Noise Aircraft Engines. ASME Turbo Expo, 6.-13. Juni 2012, Copenhagen. doi: 10.1115/GT2012-69459.

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Item URL in elib:https://elib.dlr.de/76255/
Document Type:Conference or Workshop Item (Speech)
Title:Optimised Aerodynamic Design of An OGV With Reduced Blade Count For Low Noise Aircraft Engines
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Kröger, GeorgAT-FVUNSPECIFIEDUNSPECIFIED
Schnell, RainerAT-FVUNSPECIFIEDUNSPECIFIED
Humphreys, NickRolls RoyceUNSPECIFIEDUNSPECIFIED
Date:June 2012
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI:10.1115/GT2012-69459
Status:Published
Keywords:Turbomachinery, Aerodynamics, Optimization
Event Title:ASME Turbo Expo
Event Location:Copenhagen
Event Type:international Conference
Event Dates:6.-13. Juni 2012
Organizer:ASME
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Schnell, Dr.-Ing. Rainer
Deposited On:09 Jul 2012 09:36
Last Modified:21 Jul 2023 08:21

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