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Qualitative investigation of a propeller slipstream with Background Oriented Schlieren

Roosenboom, Eric and Schröder, Andreas (2009) Qualitative investigation of a propeller slipstream with Background Oriented Schlieren. Journal of Visualization, Vol. 12 (2), pp. 165-172. Springer Verlag. DOI: 10.1007/BF03181958. ISSN 1343-8875.

Full text not available from this repository.

Official URL: http://www.vsj.or.jp/jov/

Abstract

The Background Oriented Schlieren (BOS) method has been used to qualitatively identify the (variation of) density gradients in the helical structure of a propeller slipstream. The helical structures are identified for two sideslip angles. In contrast to standard BOS correlations between exposures and a reference image, two exposures at a given time interval were cross-correlated. This revealed a more clear description of the propeller slipstream as it determines the variation of the density gradient during this interval. It enhances the visualization of the helical structure of the propeller slipstream. Based on the visualizations of the blade tip vortex trajectories the propeller slipstream contraction can be estimated.

Document Type:Article
Title:Qualitative investigation of a propeller slipstream with Background Oriented Schlieren
Authors:
AuthorsInstitution or Email of Authors
Roosenboom, EricUNSPECIFIED
Schröder, AndreasUNSPECIFIED
Date:2009
Journal or Publication Title:Journal of Visualization
Refereed publication:Yes
In Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:Vol. 12
DOI:10.1007/BF03181958
Page Range:pp. 165-172
Publisher:Springer Verlag
ISSN:1343-8875
Status:Published
Keywords:Propeller visualization, Vortical flow, Background Oriented Schlieren (BOS), Industrial wind tunnel
HGF - Research field:Aeronautics, Space and Transport
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:27 Jul 2009 10:14
Last Modified:07 Feb 2013 20:36

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