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Aerodynamic measurement technology

Klein, Christian and Konrath, Robert and Beck, Walter (2006) Aerodynamic measurement technology. AIAA – Aerospace America, December 2006, p. 22. Aerospace Measurement Technology TC contribution.

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Official URL: http://www.aiaa.org/aerospace


For the International Vortex Flow Experiment 2 (VFE-2) wind tunnel tests were carried out from the German Aerospace Center (DLR) on a 65° delta wing at sub- and transonic speeds for which the model was provided from NASA Langeley. Pressure distributions on the model surface were determined using the Pressure Sensitive Paint (PSP) technique. From these results test cases were selected for Particle Image Velocimetry (PIV) measurements to get details of the flow field. Above the delta wing with rounded leading edges a vortex system consisting of an inner and outer primary vortex could be detected and visualized, which is subject of discussion of the VFE-2 group.

Document Type:Article
Additional Information:Article / Aerospace Sciences
Title:Aerodynamic measurement technology
AuthorsInstitution or Email of Authors
Klein, ChristianUNSPECIFIED
Konrath, RobertUNSPECIFIED
Date:December 2006
Journal or Publication Title:AIAA – Aerospace America
Refereed publication:No
In ISI Web of Science:No
Volume:December 2006
Page Range:p. 22
M. Sheplak (coordinating author), UNSPECIFIED
Publisher:Aerospace Measurement Technology TC contribution
Series Name:AIAA Aerospace America - The Year in Review 2006
Keywords:Pressure Sensitive Paint (PSP), Particle Image Velocimetry (PIV), Vortex Flow Experiment
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: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Ilka Micknaus
Deposited On:06 Mar 2007
Last Modified:27 Apr 2009 13:14

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