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Flow Pattern at the Inlet of a Transonic Centrifugal Rotor

Krain, Hartmut and Hoffmann, Bettina and Beversdorff, Manfred (2007) Flow Pattern at the Inlet of a Transonic Centrifugal Rotor. International Gas Turbine Congress 2007 Tokyo, 2007-12-02 - 2007-12-07, Tokyo, Japan.

Full text not available from this repository.

Abstract

The flow field of a new, transonic centrifugal compressor rotor with 586 m/s tip speed has been analyzed experimentally and theoretically. Due to the high speed, the flow was transonic in the rotor inlet region as well as at the diffuser inlet section. The supersonic flow and the related appearance of shocks influence flow range, efficiency and pressure ratio of the machine. Detailed experimental and theoretical flow studies have been carried out in order to get deeper information about these effects. The paper mainly deals with the flow character found at the rotor inlet of the compressor. Laser measurement results and results of 3D-flow calculations are presented.

Item URL in elib:https://elib.dlr.de/49684/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Flow Pattern at the Inlet of a Transonic Centrifugal Rotor
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Krain, HartmutUNSPECIFIEDUNSPECIFIED
Hoffmann, BettinaUNSPECIFIEDUNSPECIFIED
Beversdorff, ManfredUNSPECIFIEDUNSPECIFIED
Date:August 2007
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Page Range:pp. 1-10
Series Name:Gas Turbine Society of Japan (GTSJ)
Status:Published
Keywords:Transonic centrifugal compressor, laser measurements, 3D stage calculations
Event Title:International Gas Turbine Congress 2007 Tokyo
Event Location:Tokyo, Japan
Event Type:international Conference
Event Dates:2007-12-02 - 2007-12-07
Organizer:Gas Turbine Society of Japan (GTSJ)
HGF - Research field:Energy
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L TT - Triebwerkstechnologien
DLR - Research theme (Project):L - Fan and Compressor Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: Krain, Dr.-Ing. Hartmut
Deposited On:02 Jan 2008
Last Modified:15 Jan 2010 01:10

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