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Darmstadt Rotor No. 2 - part III Experimental analysis of an aft-swept axial transonic compressor stage

Kablitz, Stephan and Bergner, Jörg and Hennecke, Dietmar K. and Beversdorff, Manfred and Schodl, Richard (2002) Darmstadt Rotor No. 2 - part III Experimental analysis of an aft-swept axial transonic compressor stage. In: Proceedings of the ISROMAC, Isromac 9 - 2002 Conference Honolulu. Isromac 9, 2002-02-10 - 2002-02-14, Honolulu.

Full text not available from this repository.

Abstract

At Darmstadt University of Technology, the Department of Gas Turbines and Flight-Propulsion operates a single stage transonic compressor test stand. Its main purpose is to provide a database for validation of CDF code. In addition, it serves as a testbed for new materials and also for the development of new measurement techniques. After setting up the test rig with a baseline rotor (Rotor No. 4) manufactured as a titanium blisk with conventional radially-stacked blade section, a new rotor (Rotor No. 2) was designed, adding considerable amounts of aft-wseep and backward lean. The new rotor's flow field and mechanical properties were investigated with various measurement techniques, including a laser-2-focus setup.

Document Type:Conference or Workshop Item (Paper)
Title:Darmstadt Rotor No. 2 - part III Experimental analysis of an aft-swept axial transonic compressor stage
Authors:
AuthorsInstitution or Email of Authors
Kablitz, StephanDarmstadt University of Technology
Bergner, JörgDarmstadt University of Technology
Hennecke, Dietmar K.Darmstadt University of Technology
Beversdorff, ManfredUNSPECIFIED
Schodl, RichardUNSPECIFIED
Date:2002
Journal or Publication Title:Proceedings of the ISROMAC, Isromac 9 - 2002 Conference Honolulu
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmail
ISROMAC 9, UNSPECIFIED
Status:Published
Keywords:axial transonic compressor, aft-sweep, laser-two-focus, gas turbines, measurement techniques, CFD code
Event Title:Isromac 9
Event Location:Honolulu
Event Type:international Conference
Event Dates:2002-02-10 - 2002-02-14
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 - Virtual Engine and Validation Methods
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Engine Measurement Systems
Deposited By:INVALID USER
Deposited On:17 Mar 2006
Last Modified:27 Apr 2009 05:03

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