The Effect of Viscosity on Hydrodynamic Stability of a Plane Flame Front

1982 ◽  
Vol 29 (3-6) ◽  
pp. 207-224 ◽  
Author(s):  
M. L. FRANKEL ◽  
G. I. SIVASHINSKY
2006 ◽  
Vol 234 ◽  
pp. S121
Author(s):  
Eusébio Z.E. Conceição ◽  
Ma Manuela J.R. Lúcio ◽  
Domingos X. Viegas

1968 ◽  
Vol 19 (1) ◽  
pp. 80-90 ◽  
Author(s):  
R. Foster ◽  
J. F. Clarke

SummaryThe wholly supersonic flow past a two-dimensional wedge is analysed on the assumption that release of chemical energy into the stream can be accomplished across a thin discontinuous plane flame front attached to the apex. Forces experienced by the wedge are calculated and representative flow patterns exhibited. Some typical interactions between the flame and shocks or centred simple waves are discussed, with emphasis on the use of pressure-flow-deflection diagrams to obtain results.


2015 ◽  
Vol 2 (1) ◽  
pp. 48-60
Author(s):  
S. Anbukumar ◽  
◽  
Munendra Kumar ◽  

2019 ◽  
Vol 489 (5) ◽  
pp. 461-464
Author(s):  
A. D. Kiverin ◽  
I. S. Yakovenko ◽  
V. E. Fortov

The problem of the detonation formation as a result of unconfined flame propagation is solved numerically. The mechanism of detonation formation is distinguished. It is related to the local formation of shock waves du- ring the linear stage of development of flame front perturbations formed on the surface of the expanding flame front. General criteria of the establishment of the conditions for the detonation transition via the proposed mechanism are formulated.


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