Application of Particle Image Velocimetry and the Background Oriented Schlieren Technique in the High-Enthalpy Shock Tunnel Göttingen
Kirmse, Tania and Agocs, Janos and Schröder, Andreas and Martinez Schramm, Jan and Karl, Sebastian and Hannemann, Klaus (2011) Application of Particle Image Velocimetry and the Background Oriented Schlieren Technique in the High-Enthalpy Shock Tunnel Göttingen. Shock Waves. Springer Verlag. DOI: 10.1007/s00193-011-0314.
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Abstract
The applicability of the particle image velocimetry (PIV) and the background-oriented schlieren (BOS) techniques in the high-enthalpy shock tunnel Göttingen of the German Aerospace Center, DLR is demonstrated. As a part of this feasibility study two different experiments are performed. The velocity field past a wedge in aMach 6 flow at a total specific enthalpy of 1.5 MJ/kg is determined by means of PIV and the results are compared to numerical predictions. The BOS technique is applied to investigate the density field in the shock layer of a sphere at 12 and 22 MJ/kg total specific enthalpies. Using a ray tracer method, the BOS results are compared to the data obtained by corresponding numerical computations.
| Document Type: | Article | ||||||||||||||
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| Additional Information: | Published online: 19. April 2011 | ||||||||||||||
| Title: | Application of Particle Image Velocimetry and the Background Oriented Schlieren Technique in the High-Enthalpy Shock Tunnel Göttingen | ||||||||||||||
| Authors: |
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| Date: | 2011 | ||||||||||||||
| Journal or Publication Title: | Shock Waves | ||||||||||||||
| Refereed publication: | Yes | ||||||||||||||
| In Open Access: | No | ||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||
| DOI: | 10.1007/s00193-011-0314 | ||||||||||||||
| Publisher: | Springer Verlag | ||||||||||||||
| Status: | Published | ||||||||||||||
| Keywords: | Particle image velocimetry (PIV), Background-oriented schlieren (BOS), Optical measurement techniques, Numerical modelling, High-enthalpy ground testing, Shock tunnel | ||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||
| HGF - Program Themes: | L AR - 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 > Spacecraft Institute of Aerodynamics and Flow Technology > Experimental Methods | ||||||||||||||
| Deposited By: | Ilka Micknaus | ||||||||||||||
| Deposited On: | 03 May 2011 15:47 | ||||||||||||||
| Last Modified: | 04 Apr 2013 16:19 |
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