Abstract
An experimental study has been conducted to examine the interaction of a shock wave and a vortex ring with a flat plate and a perforated plate. The experiments were carried out using a 30mm internal diameter shock-tube. The driver and driven gas was air. High-speed Schlieren photography was employed to study the development of the flow-field and the resulting interactions with the plates. Wall pressure measurements were also carried out to study the flow quantitatively at the exit of the shock-tube. Three different driver pressures of 4, 8 and 12bar were examined under critical driver length conditions; the shock wave Mach number was 1.33, 1.52 and 1.67, respectively.
Original language | English |
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Title of host publication | Collection of Technical Papers - 36th AIAA Fluid Dynamics Conference|Coll. Tech. Pap. AIAA Fluid Dynam. Conf. |
Pages | 115-138 |
Number of pages | 23 |
Volume | 1 |
Publication status | Published - 2006 |
Event | 36th AIAA Fluid Dynamics Confernce - San Francisco, CA Duration: 1 Jul 2006 → … |
Conference
Conference | 36th AIAA Fluid Dynamics Confernce |
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City | San Francisco, CA |
Period | 1/07/06 → … |
Keywords
- AIAA 2006-2875