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Flow Study of a Redesigned High Pressure Ratio Centrifugal Compressor

Krain, Hartmut and Hoffmann, Bettina (2008) Flow Study of a Redesigned High Pressure Ratio Centrifugal Compressor. AIAA Journal, Volume 24, Number 5, Oct. 2008, p. 7. American Institute of Aeronautics and Astronautics.

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A high specific speed, 6:1 total pressure ratio centrifugal compressor rotor has been improved by using knowledge gained from previous investigations on similar types of compressors as well as advanced 3D-design calculations.

Document Type:Article
Title:Flow Study of a Redesigned High Pressure Ratio Centrifugal Compressor
AuthorsInstitution or Email of Authors
Hoffmann, BettinaUNSPECIFIED
Date:October 2008
Journal or Publication Title:AIAA Journal
Refereed publication:Yes
In ISI Web of Science:Yes
Volume:Volume 24, Number 5, Oct. 2008
Page Range:p. 7
Publisher:American Institute of Aeronautics and Astronautics
Series Name:AIAA Journal of Propulsion and Power
Keywords:Centrifugal Compressor, 3D-calculations, laser measurements
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Fan and Compressor Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: Dr.-Ing. Hartmut Krain
Deposited On:05 Dec 2008
Last Modified:27 Apr 2009 15:32

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