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PIV Application to Transonic Axial and Radial Compressors

Voges, Melanie and Willert, Christian and Müller, Martin W. (2008) PIV Application to Transonic Axial and Radial Compressors. XIX Biannual Symposium on Measuring Techniques in Turbomachinery - Transonic and Supersonic Flow in Cascades and Turbomachines, 2008-04-07 - 2008-04-08, Rhodes-St-Genèse, Belgien.

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This paper summarizes latest DLR activities in turbomachinery research, involving the laser-based planar particle image velocimetry technique (PIV, see Raffel et al., 2007). In the first part of this contribution the experimental investigation of a single-stage transonic axial compressor equipped with casing treatment (CT) will be described. The measurements focused on the investigation of the blade tip interaction with the CT and flow phenomena occurring at the compressor's surge line. A new approach regarding light sheet introduction via periscope probe as well as a smoke-based type of seeding particles have been approved. The results obtained were subsequently used for comparison and validation of numerical calculations of the same compressor geometry performed in parallel to the experiments. The second part of this paper gives an overview on PIV measurements performed in the diffuser passage of a transonic high pressure ratio centrifugal compressor. PIV was used to analyze and further improve the understanding of the complex flow phenomena inside the vaned diffuser given the capability of capturing spatial structures.

Item URL in elib:https://elib.dlr.de/54707/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:PIV Application to Transonic Axial and Radial Compressors
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Müller, Martin W.Technische Universität DarmstadtUNSPECIFIED
Date:7 April 2008
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:PIV, transonic flow, compressor
Event Title:XIX Biannual Symposium on Measuring Techniques in Turbomachinery - Transonic and Supersonic Flow in Cascades and Turbomachines
Event Location:Rhodes-St-Genèse, Belgien
Event Type:international Conference
Event Dates:2008-04-07 - 2008-04-08
Organizer:Von Karman Institute for Fluid Dynamics
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Virtual Engine and Validation Methods (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Institute of Propulsion Technology > Engine Measurement Systems
Deposited By: Voges, Melanie
Deposited On:11 Aug 2008
Last Modified:12 Dec 2013 20:31

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