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Application of a Multimode Transition Model to Turbomachinery Flows

Kozulovic, Dragan (2007) Application of a Multimode Transition Model to Turbomachinery Flows. National Technical University of Athens.

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Abstract

A transition model is described, which is aimed at turbomachinery flow simulations and can be classified as an integral method based on experimental correlations. This model incorporates all relevant modes of transition and is calibrated on well documented test cases. Besides generic test cases, also multistage turbomachinery configurations are presented, clearly demonstrating the high accuracy of viscous loss predictions. Hence, the presented approach can be used as a tool for the industrial aerodynamic design of highly loaded turbomachinery components.

Item URL in elib:https://elib.dlr.de/47646/
Document Type:Editorship of Proceedings
Title:Application of a Multimode Transition Model to Turbomachinery Flows
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Kozulovic, DraganUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:5 March 2007
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:7
Number of Pages:1369
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Papailiou, K. D.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Martelli, F.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Manna, M.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Publisher:National Technical University of Athens
Status:Published
Keywords:transition modelling, turbomachinery flow
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 - Virtual Engine and Validation Methods (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Numerical Methodes
Deposited By: Kozulovic, Dragan
Deposited On:19 Mar 2007
Last Modified:24 Apr 2024 19:09

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