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MODELLING TRANSITION FOR THE DESIGN OF MODERN AXIAL TURBOMACHINES

Marciniak, Vincent and Weber, Anton and Kügeler, Edmund (2014) MODELLING TRANSITION FOR THE DESIGN OF MODERN AXIAL TURBOMACHINES.

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Official URL: http://www.wccm-eccm-ecfd2014.org/

Abstract

The aim of this paper is to investigate whether or not a correlation-based transition model can be used for the design of multistage turbomachinery components. To this end, two components, a low-pressure turbine and an axial compressor, are computed at design and o�-design conditions. The results of the steady computations are compared with experimental data in terms of overall performance and transition occurrence. In all cases, the agreement between the measurements and the computations is good, meaning that the computational setup can be used in a multistage turbomachinery context.

Item URL in elib:https://elib.dlr.de/90279/
Document Type:Proceedings
Title:MODELLING TRANSITION FOR THE DESIGN OF MODERN AXIAL TURBOMACHINES
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Marciniak, Vincentvincent.marciniak (at) dlr.deUNSPECIFIED
Weber, Antonanton.weber (at) dlr.deUNSPECIFIED
Kügeler, Edmundedmund.kuegeler (at) dlr.deUNSPECIFIED
Date:July 2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:12
Editors:
EditorsEmail
Onate, E.UNSPECIFIED
Oliver, J.UNSPECIFIED
Huerta, A.UNSPECIFIED
Status:Published
Keywords:Transition Modelling, Turbomachine, Multistage, Compressor, Turbine
HGF - Research field:Energy
HGF - Program:Efficient Energy Conversion and Use (old)
HGF - Program Themes:Power Plants (old)
DLR - Research area:Energy
DLR - Program:E VG - Combustion and Gas Turbine Technologies
DLR - Research theme (Project):E - Gas Turbine (old), L - Fan and Compressor Technologies, L - Turbine Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Numerical Methodes
Deposited By: Marciniak, Vincent
Deposited On:18 Aug 2014 10:41
Last Modified:18 Aug 2014 10:41

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