Encyclopedia of Computational Mechanics Second Edition 2017
DOI: 10.1002/9781119176817.ecm2067
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Combustion

Abstract: This chapter describes the basic phenomena controlling reacting flows and the corresponding computational methodologies. Combustion regimes (premixed or diffusion flames, laminar or turbulent cases, stable or unstable behavior) are first defined before introducing the basic terminology required to understand numerical techniques for reacting flows. The governing equations for combustion are more complex than those used in classical aerodynamics, and their specificities are discussed before describing numerical… Show more

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Cited by 20 publications
(25 citation statements)
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“…where h s,k is the specific enthalpy of the k th species, p the pressure, τ ki the viscous shear stress, ẇT = | ẇF |H the source term originating from heat release (due to combustion henceforth referred to the heat release rate) with H being the heating value of the fuel, 53 and e = C V T + u k u k / 2 the specific stagnation internal energy. For the current analysis the term…”
Section: Mathematical Backgroundmentioning
confidence: 99%
“…where h s,k is the specific enthalpy of the k th species, p the pressure, τ ki the viscous shear stress, ẇT = | ẇF |H the source term originating from heat release (due to combustion henceforth referred to the heat release rate) with H being the heating value of the fuel, 53 and e = C V T + u k u k / 2 the specific stagnation internal energy. For the current analysis the term…”
Section: Mathematical Backgroundmentioning
confidence: 99%
“…The EDM was introduced by Magnussen and Hjertager ( 12 , 28 ) . It assumes that fuel and oxidiser are carried by separate eddies in diffusion flames.…”
Section: Numerical Modelling Of Scramjetsmentioning
confidence: 99%
“…In the above equation, s is the mass stoichiometric ratio defined as and equals 8 for H 2 –air combustion ( 28 ) , W s is the molar mass in kg/mol and is the mass fraction. In Equation (6), β * is a turbulence model constant with a value of 0.09 and ω (1/s) is the specific dissipation of turbulent kinetic energy obtained through the turbulence model.…”
Section: Numerical Modelling Of Scramjetsmentioning
confidence: 99%
“…All experiments investigation was founded on the basis of authors [6][7][8][9][10][11][12][13]. Two pellet boilers of different manufacturers of the same heating power (40 kW), equipped with a horizontally feed burners were used to perform the measurements in the present study.…”
Section: Experiments Datamentioning
confidence: 99%