Abstract
The present study involves the application of a Pressure-Sensitive Paint (Tris-Bathophen- anthroline Ruthenium Perchlorate), incorporated in a recipe developed in-house at Aero-Physics Laboratory (APL) based in The University of Manchester, to three separate ex- perimental setups. The first is to map the flow field on the sidewall of a complex geometry. This model is divided into three main sections: a converging concave section, an area of uniform cross-section which leads to the third section which is bound by solid straight walls on the top and bottom surfaces. The inlet pressure was varied in the range 1 - 3 bar. The second and third cases took part in a transonic wind tunnel and are comprised of: firstly, the examination of the control effectiveness of dimples on the glancing shock wave turbulent boundary layer interaction produced by a series of hemi-cylindrically blunt fins at Mach 0.8, and secondly, the well known symmetrical diamond-wedge airfoil at Mach 1.4. Copyright © 2008 by H. Zare-Behtash, K. Kontis.
| Original language | English |
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| Title of host publication | 46th AIAA Aerospace Sciences Meeting and Exhibit|AIAA Aerosp. Sci. Meet. Exhib. |
| Publication status | Published - 2008 |
| Event | 46th AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV Duration: 1 Jul 2008 → … |
Conference
| Conference | 46th AIAA Aerospace Sciences Meeting and Exhibit |
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| City | Reno, NV |
| Period | 1/07/08 → … |
Keywords
- AIAA-2008-355