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Flow Analysis in a Transonic Centrifugal Compressor Rotor Using 3-Component Laser Velocimetry
Krain, H. and Karpinski, G. and Beversdorff, M. (2001) Flow Analysis in a Transonic Centrifugal Compressor Rotor Using 3-Component Laser Velocimetry. In: ASME Turbo Expo 2001, pp. 1-12. The American Society of Mechanical Engineers, Atlanta, USA. ASME-Tagung, New Orleans, USA, June 2001.
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Abstract
The flow conditions found inside a transonic high pressure ratio centrifugal compressor rotor operated with a tip speed of 586 m/s are described. A 3-component Laser velocimeter was used for the optical measurements.
| Document Type: | Conference or Workshop Item (Paper) | ||||||||
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| Additional Information: | LIDO-Berichtsjahr=2001, monograph_id=2001-6T-315, | ||||||||
| Title: | Flow Analysis in a Transonic Centrifugal Compressor Rotor Using 3-Component Laser Velocimetry | ||||||||
| Authors: |
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| Date: | 2001 | ||||||||
| Journal or Publication Title: | ASME Turbo Expo 2001 | ||||||||
| Page Range: | pp. 1-12 | ||||||||
| Editors: |
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| Publisher: | The American Society of Mechanical Engineers, Atlanta, USA | ||||||||
| Status: | Published | ||||||||
| Keywords: | Centrifugal Compressor, Laser | ||||||||
| Event Title: | ASME-Tagung, New Orleans, USA, June 2001 | ||||||||
| Organizer: | ASME | ||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||
| HGF - Program: | Aeronautics | ||||||||
| HGF - Program Themes: | L - no assignement | ||||||||
| DLR - Research area: | Aeronautics | ||||||||
| DLR - Program: | L TT - Triebwerkstechnologien | ||||||||
| DLR - Research theme (Project): | L - Fan and Compressor Technologies | ||||||||
| Location: | Köln-Porz | ||||||||
| Institutes and Institutions: | Institute of Propulsion Technology | ||||||||
| Deposited By: | elib DLR-Beauftragter | ||||||||
| Deposited On: | 16 Sep 2005 | ||||||||
| Last Modified: | 06 Jan 2010 13:16 |
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