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Generation of adverse pressure gradient in the circumferential flashback of a premixed flame

Generation of adverse pressure gradient in the circumferential flashback of a premixed flame
Generation of adverse pressure gradient in the circumferential flashback of a premixed flame
Circumferential upstream propagation of a premixed flame in a region confined between two concentric tubes is considered. The cold flow in this configuration features rotational motion and the flame is modelled as an interface separating the burned and unburned gases. Through an analytical solution of the integral form of the governing equations, it is shown that the static pressure increases across the flame. Hence, the circumferential propagation of the flame is associated with the generation of an adverse pressure gradient. The theoretical prediction of the pressure increase is, further, supported by the experimental observations and discussed in the context of the theory of flame back pressure. The results extend the recent findings on the generation of adverse pressure gradient during the axial propagation of swirling flames, to the circumferential direction. It is argued that the demonstrated pressure gain across the flame can significantly facilitate flame flashback.
1386-6184
663–687
Karimi, N.
620646d6-27c9-4e1e-948f-f23e4a1e773a
McGrath, S.
6622aec5-ea9f-45fb-8696-59844e3ab783
Brown, P.
8b4b4591-6932-4d1a-b528-4a8370d7dad9
Weinkauff, J.
3d4b19ff-bbeb-4700-aaaf-910e921c9b1a
Dreizler, A.
f5447932-c3ed-4c5b-b36c-5878ef8181e7
Karimi, N.
620646d6-27c9-4e1e-948f-f23e4a1e773a
McGrath, S.
6622aec5-ea9f-45fb-8696-59844e3ab783
Brown, P.
8b4b4591-6932-4d1a-b528-4a8370d7dad9
Weinkauff, J.
3d4b19ff-bbeb-4700-aaaf-910e921c9b1a
Dreizler, A.
f5447932-c3ed-4c5b-b36c-5878ef8181e7

Karimi, N., McGrath, S., Brown, P., Weinkauff, J. and Dreizler, A. (2016) Generation of adverse pressure gradient in the circumferential flashback of a premixed flame. Flow, Turbulence and Combustion, 97, 663–687. (doi:10.1007/s10494-015-9695-0).

Record type: Article

Abstract

Circumferential upstream propagation of a premixed flame in a region confined between two concentric tubes is considered. The cold flow in this configuration features rotational motion and the flame is modelled as an interface separating the burned and unburned gases. Through an analytical solution of the integral form of the governing equations, it is shown that the static pressure increases across the flame. Hence, the circumferential propagation of the flame is associated with the generation of an adverse pressure gradient. The theoretical prediction of the pressure increase is, further, supported by the experimental observations and discussed in the context of the theory of flame back pressure. The results extend the recent findings on the generation of adverse pressure gradient during the axial propagation of swirling flames, to the circumferential direction. It is argued that the demonstrated pressure gain across the flame can significantly facilitate flame flashback.

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More information

Published date: 6 January 2016

Identifiers

Local EPrints ID: 508889
URI: http://eprints.soton.ac.uk/id/eprint/508889
ISSN: 1386-6184
PURE UUID: e978ad16-18e3-468a-a5d8-92e6d6a8fb5b
ORCID for N. Karimi: ORCID iD orcid.org/0000-0002-4559-6245

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Date deposited: 05 Feb 2026 17:50
Last modified: 06 Feb 2026 03:12

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Contributors

Author: N. Karimi ORCID iD
Author: S. McGrath
Author: P. Brown
Author: J. Weinkauff
Author: A. Dreizler

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