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Feasibility study: Helicopter Blade Tip Vortex Positions measured in free flight by means of stereoscopic Background Oriented Schlieren Method (BOS)

Klinge, Falk and Hecklau, Martin and Kompenhans, Jürgen and Göhmann, Uwe (2006) Feasibility study: Helicopter Blade Tip Vortex Positions measured in free flight by means of stereoscopic Background Oriented Schlieren Method (BOS). Society of Flight Test Engineers, 17th European Chapter Symposium 2006, 2006-06-12 - 2006-06-14, Amsterdam (The Netherlands).

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Abstract

During a measurement with a MMB Bo 105 in Braunschweig, the rotor blade tip vortex position was investigated by means of stereoscopic BOS

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Feasibility study: Helicopter Blade Tip Vortex Positions measured in free flight by means of stereoscopic Background Oriented Schlieren Method (BOS)
Authors:
AuthorsInstitution or Email of Authors
Klinge, FalkUNSPECIFIED
Hecklau, MartinUNSPECIFIED
Kompenhans, JürgenUNSPECIFIED
Göhmann, UweUNSPECIFIED
Date:2006
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-12
Series Name:CD-ROM Proceedings
Status:Published
Keywords:BOS, helicopter rotor blade tip vortex, position
Event Title:Society of Flight Test Engineers, 17th European Chapter Symposium 2006
Event Location:Amsterdam (The Netherlands)
Event Type:international Conference
Event Dates:2006-06-12 - 2006-06-14
Organizer:SFTE/NLR
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Braunschweig , Göttingen
Institutes and Institutions:Flight Operations > Flight Facility Braunschweig
Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Ilka Micknaus
Deposited On:13 Nov 2006
Last Modified:27 Apr 2009 05:00

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