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Influence of Blade Tip Clearances on Loss Mechanisms in Different High-Pressure Turbine Configurations

Ullrich, Wolfram (2012) Influence of Blade Tip Clearances on Loss Mechanisms in Different High-Pressure Turbine Configurations. Other, Institute für Antriebstechnik.

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Item URL in elib:https://elib.dlr.de/83093/
Document Type:Thesis (Other)
Title:Influence of Blade Tip Clearances on Loss Mechanisms in Different High-Pressure Turbine Configurations
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Ullrich, WolframAT-TUUNSPECIFIED
Date:31 January 2012
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:93
Status:Published
Keywords:CFD-Simulation, Numerische Strömungsmechanik, Verlustkoeffizienten, Spaltverluste, Turbine, Turbulenz
Institution:Institute für Antriebstechnik
Department:Turbine
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 - Turbine Technologies (old)
Location: Göttingen
Institutes and Institutions:Institute of Propulsion Technology > Turbine
Deposited By: Giess, Dr.-Ing. Peter-Anton
Deposited On:25 Jun 2013 14:59
Last Modified:25 Jun 2013 14:59

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