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Head-on collision of shock wave induced vortices with solid and perforated walls

Head-on collision of shock wave induced vortices with solid and perforated walls
Head-on collision of shock wave induced vortices with solid and perforated walls
An experimental study has been conducted to examine the interaction of shock wave induced vortices with a flat plate and a perforated plate. The experiments were carried out using a internal diameter shock-tube at Mach numbers 1.31, 1.49, and 1.61 under critical driver conditions. Air was used both in the driver and driven sections. High-speed schlieren photography was employed to study the flow development and the resulting interactions with the plates. Wall pressure measurements on both plates were also carried out in order to study the flow interactions quantitatively. The experimental results indicated that a region of strong flow development is generated near the wall surface, due to the flow interactions of reflected waves and oncoming induced vortices. This flow behavior causes the generation of multiple pressure fluctuations on the wall. In the case of the perforated plate, a weaker initial reflected wave is produced, which is followed by compression waves, due to the internal reflections within the plate. The transmitted wave is reduced in strength, compared to the initial incident shock wave.
1070-6631
Kontis, K.
e40ecdbc-e5e9-4522-abf9-e3c3f3c2d7fa
Zare-Behtash, H.
74be9b97-cb09-49c6-9f75-7ec58c0dd16c
Kounadis, D.
56b64eb9-c731-477f-92f9-d87fac867ef6
Kontis, K.
e40ecdbc-e5e9-4522-abf9-e3c3f3c2d7fa
Zare-Behtash, H.
74be9b97-cb09-49c6-9f75-7ec58c0dd16c
Kounadis, D.
56b64eb9-c731-477f-92f9-d87fac867ef6

Kontis, K., Zare-Behtash, H. and Kounadis, D. (2008) Head-on collision of shock wave induced vortices with solid and perforated walls. Physics of Fluids, 20, [016104]. (doi:10.1063/1.2837172).

Record type: Article

Abstract

An experimental study has been conducted to examine the interaction of shock wave induced vortices with a flat plate and a perforated plate. The experiments were carried out using a internal diameter shock-tube at Mach numbers 1.31, 1.49, and 1.61 under critical driver conditions. Air was used both in the driver and driven sections. High-speed schlieren photography was employed to study the flow development and the resulting interactions with the plates. Wall pressure measurements on both plates were also carried out in order to study the flow interactions quantitatively. The experimental results indicated that a region of strong flow development is generated near the wall surface, due to the flow interactions of reflected waves and oncoming induced vortices. This flow behavior causes the generation of multiple pressure fluctuations on the wall. In the case of the perforated plate, a weaker initial reflected wave is produced, which is followed by compression waves, due to the internal reflections within the plate. The transmitted wave is reduced in strength, compared to the initial incident shock wave.

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More information

Accepted/In Press date: 24 November 2007
Published date: 31 January 2008

Identifiers

Local EPrints ID: 493194
URI: http://eprints.soton.ac.uk/id/eprint/493194
ISSN: 1070-6631
PURE UUID: 4b5f6855-412b-4d9c-927c-cf130b756df7
ORCID for H. Zare-Behtash: ORCID iD orcid.org/0000-0002-4769-4076

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Date deposited: 27 Aug 2024 16:56
Last modified: 28 Aug 2024 02:16

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Contributors

Author: K. Kontis
Author: H. Zare-Behtash ORCID iD
Author: D. Kounadis

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