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.
Full text not available from this repository.
Abstract
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.
Item URL in elib: | https://elib.dlr.de/56452/ | ||||||||||||
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Document Type: | Article | ||||||||||||
Title: | Flow Study of a Redesigned High Pressure Ratio Centrifugal Compressor | ||||||||||||
Authors: |
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Date: | October 2008 | ||||||||||||
Journal or Publication Title: | AIAA Journal | ||||||||||||
Refereed publication: | Yes | ||||||||||||
Open Access: | No | ||||||||||||
Gold Open Access: | No | ||||||||||||
In SCOPUS: | No | ||||||||||||
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 | ||||||||||||
Status: | Published | ||||||||||||
Keywords: | Centrifugal Compressor, 3D-calculations, laser measurements | ||||||||||||
HGF - Research field: | Aeronautics, Space and Transport (old) | ||||||||||||
HGF - Program: | Aeronautics | ||||||||||||
HGF - Program Themes: | Propulsion Systems (old) | ||||||||||||
DLR - Research area: | Aeronautics | ||||||||||||
DLR - Program: | L ER - Engine Research | ||||||||||||
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: | 05 Dec 2008 | ||||||||||||
Last Modified: | 27 Apr 2009 15:32 |
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