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Visualization of Secondary Flow Structures Caused by Rotating Instability: Synchronized Stereo High-Speed PIV and Unsteady Pressure Measurements

Pardowitz, Benjamin and Peter, Julija and Tapken, Ulf and Thamsen, Paul Uwe and Enghardt, Lars (2015) Visualization of Secondary Flow Structures Caused by Rotating Instability: Synchronized Stereo High-Speed PIV and Unsteady Pressure Measurements. In: The American Institute of Aeronautics and Astronautics (AIAA). 45th AIAA Fluid Dynamics Conference, 22.-26. Juni 2015, Dallas, USA.

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Item URL in elib:https://elib.dlr.de/101012/
Document Type:Conference or Workshop Item (Speech)
Additional Information:Paper-ID: 2150985
Title:Visualization of Secondary Flow Structures Caused by Rotating Instability: Synchronized Stereo High-Speed PIV and Unsteady Pressure Measurements
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Pardowitz, BenjaminBenjamin.Pardowitz (at) dlr.deUNSPECIFIED
Peter, Julijajulija.peter (at) tu-berlin.deUNSPECIFIED
Tapken, Ulfulf.tapken (at) dlr.deUNSPECIFIED
Thamsen, Paul UweTU-Berlin / Paul-Uwe.Thamsen (at) tu-berlin.deUNSPECIFIED
Enghardt, Larslars.enghardt (at) dlr.deUNSPECIFIED
Date:22 June 2015
Journal or Publication Title:The American Institute of Aeronautics and Astronautics (AIAA)
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:High Speed Stereo PIV, rotating instability, compressor, unsteady aerodynamics, near stall, modal waves, vortex structures
Event Title:45th AIAA Fluid Dynamics Conference
Event Location:Dallas, USA
Event Type:international Conference
Event Dates:22.-26. Juni 2015
Organizer:The American Institute of Aeronautics and Astronautics (AIAA)
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:propulsion systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Fan and Compressor Technologies
Location: Berlin-Charlottenburg
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Pardowitz, Benjamin
Deposited On:06 Jan 2016 11:30
Last Modified:10 May 2016 23:38

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