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Unsteady Vortex Behaviour of a Rotating 65° Delta Wing Using Pressure Sensitive Paint (PSP)

Klein, Christian and Sachs, Werner and Henne, Ulrich and Engler, Rolf and Egami, Yasuhiro and Ondrus, V. (2006) Unsteady Vortex Behaviour of a Rotating 65° Delta Wing Using Pressure Sensitive Paint (PSP). 12th International Symposium on Flow Visualization, 2006-09-10 - 2006-09-14, Göttingen (Germany).

Full text not available from this repository.

Abstract

Visualization and measurements of aerodynamic effects on a delta-wing model were conducted using an optical pressure measurement system, based on the pressure-sensitive paint (PSP) technique. A special 65° delta wing, the so called DLR-PSP model, was tested in the transonic wind tunnel DNW-TWG in Göttingen. A rolling apparatus was built up to enable roll rates up to 10 Hz. The experiments were carried out at angles-of-attack up to alpha = 17° at Ma = 0.8. For this rotating model an unsteady PSP technique was successfully applied.

Document Type:Conference or Workshop Item (Speech)
Additional Information:30 Folien, Vortrag nicht auf CD
Title:Unsteady Vortex Behaviour of a Rotating 65° Delta Wing Using Pressure Sensitive Paint (PSP)
Authors:
AuthorsInstitution or Email of Authors
Klein, ChristianUNSPECIFIED
Sachs, WernerUNSPECIFIED
Henne, UlrichUNSPECIFIED
Engler, RolfUNSPECIFIED
Egami, YasuhiroUNSPECIFIED
Ondrus, V.Uni Hohenheim
Date:2006
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:CD ROM Proceedings
Status:Published
Keywords:Unsteady PSP, 65° delta-wing model
Event Title:12th International Symposium on Flow Visualization
Event Location:Göttingen (Germany)
Event Type:international Conference
Event Dates:2006-09-10 - 2006-09-14
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:30 Nov 2006
Last Modified:27 Apr 2009 13:14

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