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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.

Full text not available from this repository.

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)
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:
AuthorsInstitution or Email of Authors
Krain, H.UNSPECIFIED
Karpinski, G.UNSPECIFIED
Beversdorff, M.UNSPECIFIED
Date:2001
Journal or Publication Title:ASME Turbo Expo 2001
Page Range:pp. 1-12
Editors:
EditorsEmail
ASME, UNSPECIFIED
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 (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
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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