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Development of stereoscopic Background Oriented Schlieren Method (BOS) and Laser Light Sheet technique (LLS) for study of Reynolds number effects on wing tip vortex positions under cryogenic conditions

Klinge, Falk and Pallek, Dieter and Kompenhans, Jürgen (2006) Development of stereoscopic Background Oriented Schlieren Method (BOS) and Laser Light Sheet technique (LLS) for study of Reynolds number effects on wing tip vortex positions under cryogenic conditions. 13th International Symposium on Applications of Laser Techniques to Fluid Mechanics, 2006-06-26 - 2006-06-29, Lisbon (Portugal).

Full text not available from this repository.

Abstract

During a measurement at the ETW in Köln the position of a wing tip vortex was investigated by means of stereoscopic BOS and Laser light sheet technique under cryogenic conditions.

Item URL in elib:https://elib.dlr.de/22478/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Development of stereoscopic Background Oriented Schlieren Method (BOS) and Laser Light Sheet technique (LLS) for study of Reynolds number effects on wing tip vortex positions under cryogenic conditions
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Klinge, FalkUNSPECIFIEDUNSPECIFIED
Pallek, DieterUNSPECIFIEDUNSPECIFIED
Kompenhans, JürgenUNSPECIFIEDUNSPECIFIED
Date:2006
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:vortex, Laser light sheet technique, cryogenic, ETW, BOS, Reynolds number effect, wing tip vortex position
Event Title:13th International Symposium on Applications of Laser Techniques to Fluid Mechanics
Event Location:Lisbon (Portugal)
Event Type:international Conference
Event Dates:2006-06-26 - 2006-06-29
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Micknaus, Ilka
Deposited On:16 Nov 2006
Last Modified:27 Apr 2009 05:01

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