DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Contact | Deutsch
Fontsize: [-] Text [+]

Development of PSP Technique for Application on the VFE-2 65° Delta Wing Configuration

Klein, Christian and Sachs, Werner and Henne, Ulrich and Engler, Rolf and Wiedemann, Andreas and Konrath, Robert (2006) Development of PSP Technique for Application on the VFE-2 65° Delta Wing Configuration. 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006-01-09 - 2006-01-12, Reno, Nevada (USA). ISBN 1-56347-795-5.

Full text not available from this repository.

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


For the International Vortex Flow Experiment 2 (VFE-2) new wind tunnel tests on a NASA delta-wing model by using modern non-intrusive measurement techniques have been performed in the DNW-TWG (Göttingen) transonic wind tunnel. In order to obtain a good understanding of the flow around the wind tunnel model the PSP (Pressure Sensitive Paint) technique has been applied. The PSP technique can be used to realize absolute pressure measurements on the whole surface of a model using scientific grade cameras and advanced image processing techniques. By means of the planar pressure information of the flow topology can be investigated in more detail than would be possible with data of conventional pressure taps. Surface pressures on the entire surface of the model have been obtained using DLR's mobile PSP system, viewing from top and bottom by means of four CCD-cameras. Finally, the measured pressures have been integrated to calculate forces and moments of the full model.

Document Type:Conference or Workshop Item (Speech, Paper)
Additional Information: LIDO-Berichtsjahr=2006 5 Disc, CD Code: 778-241002 36 Folien
Title:Development of PSP Technique for Application on the VFE-2 65° Delta Wing Configuration
AuthorsInstitution or Email of Authors
Klein, ChristianUNSPECIFIED
Wiedemann, AndreasCB-Network, Bremen
Konrath, RobertUNSPECIFIED
Refereed publication:No
In ISI Web of Science:No
Volume:Vol. 11, No. 1-5
Series Name:AIAA Meeting Papers on Disc
Keywords:Vortex Flow Experiment 2 (VFE-2), PSP (Pressure Sensitive Paint)
Event Title:44th AIAA Aerospace Sciences Meeting and Exhibit
Event Location:Reno, Nevada (USA)
Event Type:international Conference
Event Dates:2006-01-09 - 2006-01-12
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:19 Jun 2006
Last Modified:27 Apr 2009 04:56

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.