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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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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.
| 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 | ||||||
| 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 | ||||||
| HGF - Program: | Aeronautics | ||||||
| HGF - Program Themes: | L ER - Engine Research | ||||||
| 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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