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.
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)|
|In ISI Web of Science:||No|
|Series Name:||CD ROM Proceedings|
|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|
|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|
Repository Staff Only: item control page