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Transverse jet-cavity interactions with the influence of an impinging shock

Transverse jet-cavity interactions with the influence of an impinging shock
Transverse jet-cavity interactions with the influence of an impinging shock
For high-speed air breathing engines, fuel injection and subsequent mixing with air is paramount for combustion. The high freestream velocity poses a great challenge to efficient mixing both in macroscale and microscale. Utilising cavities downstream of fuel injection locations, as a means to hold the flow and stabilise the combustion, is one mechanism which has attracted much attention, requiring further research to study the unsteady flow features and interactions occurring within the cavity. In this study we combine the transverse jet injection upstream of a cavity with an impinging shock to see how this interaction influences the cavity flow, since impinging shocks have been shown to enhance mixing of transverse jets. Utilising qualitative and quantitative methods: schlieren, oilflow, PIV, and PSP the induced flowfield is analysed. The impinging shock lifts the shear layer over the cavity and combined with the instabilities generated by the transverse jet creates a highly complicated flowfield with numerous vertical structures. The interaction between the oblique shock and the jet leads to a relatively uniform velocity distribution within the cavity.
0142-727X
146-155
Zare-Behtash, H.
74be9b97-cb09-49c6-9f75-7ec58c0dd16c
Lo, K.H.
e2fcd08c-2efd-4cec-ad0a-92969e9d1139
Kontis, K.
e40ecdbc-e5e9-4522-abf9-e3c3f3c2d7fa
Ukai, T.
b83787a3-b48e-4c83-8ad1-9d6c15ef8a7b
Obayashi, S.
f5569406-1354-4642-82c3-82bf73c6594e
Zare-Behtash, H.
74be9b97-cb09-49c6-9f75-7ec58c0dd16c
Lo, K.H.
e2fcd08c-2efd-4cec-ad0a-92969e9d1139
Kontis, K.
e40ecdbc-e5e9-4522-abf9-e3c3f3c2d7fa
Ukai, T.
b83787a3-b48e-4c83-8ad1-9d6c15ef8a7b
Obayashi, S.
f5569406-1354-4642-82c3-82bf73c6594e

Zare-Behtash, H., Lo, K.H., Kontis, K., Ukai, T. and Obayashi, S. (2015) Transverse jet-cavity interactions with the influence of an impinging shock. International Journal of Heat and Fluid Flow, 53, 146-155. (doi:10.1016/j.ijheatfluidflow.2015.03.004).

Record type: Article

Abstract

For high-speed air breathing engines, fuel injection and subsequent mixing with air is paramount for combustion. The high freestream velocity poses a great challenge to efficient mixing both in macroscale and microscale. Utilising cavities downstream of fuel injection locations, as a means to hold the flow and stabilise the combustion, is one mechanism which has attracted much attention, requiring further research to study the unsteady flow features and interactions occurring within the cavity. In this study we combine the transverse jet injection upstream of a cavity with an impinging shock to see how this interaction influences the cavity flow, since impinging shocks have been shown to enhance mixing of transverse jets. Utilising qualitative and quantitative methods: schlieren, oilflow, PIV, and PSP the induced flowfield is analysed. The impinging shock lifts the shear layer over the cavity and combined with the instabilities generated by the transverse jet creates a highly complicated flowfield with numerous vertical structures. The interaction between the oblique shock and the jet leads to a relatively uniform velocity distribution within the cavity.

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More information

Accepted/In Press date: 26 March 2015
e-pub ahead of print date: 11 April 2015

Identifiers

Local EPrints ID: 491697
URI: http://eprints.soton.ac.uk/id/eprint/491697
ISSN: 0142-727X
PURE UUID: 8b4af083-544f-4145-9aa0-67f4b9d83ab3
ORCID for H. Zare-Behtash: ORCID iD orcid.org/0000-0002-4769-4076

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Date deposited: 03 Jul 2024 16:03
Last modified: 11 Jul 2024 02:18

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Contributors

Author: H. Zare-Behtash ORCID iD
Author: K.H. Lo
Author: K. Kontis
Author: T. Ukai
Author: S. Obayashi

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