Plane combustion wave

Piane Combustion Wave. See Combustion Wave Propagation in Vol 3, C433-R Ref J.H. Burgoyne F. Weinberg, A Method of Analysis of a plane Combustion Wave , 4th SyropGombstn, Williams Wilkins, Baltimore (1953), 294-302. ... 

A unified statistical model for premixed turbulent combustion and its subsequent application to predict the speed of propagation and the stmcture of plane turbulent combustion waves is available (29—32). 

MAF 24, 443-50(1950) CA 45, 8772(1951) (Present state and value of the hydrothermo-dynamic theory of explosions and shocks, I. The plane shock waves compressibility by shock without combustion) 17) Ibid 25, 421-624 923-1006(1951) (Thickness of shock waves and mechanism of inflammation in combustion waves) 18) T. VonKarmdn, Termotecnica (Milan) 5(2),... 

The quantity, h, in Equation 5 is not likely to be greatly different from its value in a plane adiabatic combustion wave. Taking x as the coordinate normal to such wave, h becomes the integral of the excess enthalpy per unit volume along the x-axis, so that the differential quotient, dh/dx, represents the excess enthalpy per unit volume in any layer, dx. Assuming the layer to be fixed with respect to a reference point on the x-axis, the mass flow passes through the layer in the direction from the unbumed, w, to the burned, 6, side at a velocity, S, transporting enthalpy at the rate Sdh/dx. Because the wave is in the steady state, heat flows by conduction at the same rate in the opposite direction, so that... 

If we consider a combustion wave as an infinite plane moving through a reaction system, then with respect to the plane itself considered as stationary the unburiied gases move toward it at a velocity while far behind it the burned gases leave with a velocity Vh- The difference in velocities is due to the difference in densities of the burned and unburned gases, p and pw. The law of conservation of mass requires that the mass flow rate across any surface be constant, so that, if v is the linear gas velocity at any point with reference to the stationary flame front, the mass velocity Th = pv constant at every point and, in particular, far from the flame front on either side... 

Bartlma, F., and K. Schroder. 1986. The diffraction of a plane detonation wave at a convex corner. Combustion Flame 66 237-48. 

Dynamics of combustion products behind plane and spherical detonation wave fronts in explosives )... 

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