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Measurement of the position of rotor blade vortices generated by a helicopter in free flight by means of stereoscopic Background Oriented Schlieren Method (BOS)

Klinge, Falk and Hecklau, Martin and Raffel, Markus and Kompenhans, Jürgen and Göhmann, Uwe (2006) Measurement of the position of rotor blade vortices generated by a helicopter in free flight by means of stereoscopic Background Oriented Schlieren Method (BOS). 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 with a MMB Bo 105 in Braunschweig, the rotor blade tip vortex position was investigated by means of stereoscopic BOS

Item URL in elib:https://elib.dlr.de/22479/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Measurement of the position of rotor blade vortices generated by a helicopter in free flight by means of stereoscopic Background Oriented Schlieren Method (BOS)
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Klinge, FalkUNSPECIFIEDUNSPECIFIED
Hecklau, MartinUNSPECIFIEDUNSPECIFIED
Raffel, MarkusUNSPECIFIEDUNSPECIFIED
Kompenhans, JürgenUNSPECIFIEDUNSPECIFIED
Göhmann, UweUNSPECIFIEDUNSPECIFIED
Date:2006
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-12
Series Name:Conference Proceedings
Status:Published
Keywords:Helicopter rotor blade tip vortex position, BOS
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: Braunschweig , Göttingen
Institutes and Institutions:Flight Operations > Flight Facility Braunschweig
Institute of Aerodynamics and Flow Technology > Helicopters
Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Micknaus, Ilka
Deposited On:13 Nov 2006
Last Modified:27 Apr 2009 05:01

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