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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

Abstract

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.

Item URL in elib:https://elib.dlr.de/45434/
Document Type:Article
Additional Information:Article / Aerospace Sciences
Title:Aerodynamic measurement technology
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Klein, ChristianUNSPECIFIEDUNSPECIFIED
Konrath, RobertUNSPECIFIEDUNSPECIFIED
Beck, WalterUNSPECIFIEDUNSPECIFIED
Date:December 2006
Journal or Publication Title:AIAA – Aerospace America
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:December 2006
Page Range:p. 22
Editors:
EditorsEmail
M. Sheplak (coordinating author), UNSPECIFIED
Publisher:Aerospace Measurement Technology TC contribution
Series Name:AIAA Aerospace America - The Year in Review 2006
Status:Published
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 (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:06 Mar 2007
Last Modified:27 Apr 2009 13:14

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