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266  Dust Explosions in the Process Industries

               The linear rate at which a laminar combustion wave or reaction zone propagates rel-
             ative to the unburned gas of a flammable mixture is called thefundamental or laminar
             burning velocity, commonly denoted S,. As pointed out by Kuchta (1985), this velocity
             is a fundamentalproperty of the mixture and depends primarily on the thermal diffusivity
             A/pC, of the unburned gas, where A is the thermal conductivity, p is the density, and C,
             is the specific heat at constant pressure of the unburned gas, and on the chemical reac-
             tion rate and heat of combustion of the gas. The reaction zone in a premixed gas is nor-
             mally quite thin, on the order of  1  111111.According to the classical Mallard-le Chatelier
             (1883) theory, the fundamental laminar burning velocity of a homogeneous gas mixture
             equals


                                                                                    (4.16)


             where Tiis the ignition temperature of the gas mixture and L is the thickness of the reac-
             tion zone. One problem with this theory is that a relevant value of Tiis normally not known
             for a given gas mixture. The fundamental limitation of the theory is that it does not relate
             S, to the heat release rate. Therefore, more refined theories have been developed, as are
             mentioned here.
               Of great practical interest is the flame speedS’   that is, the speed of the flame front rel-
             ative to an observer or fixed geometries. It may be defined as

             Sf = S, +S,                                                            (4.17)

             where S, is the gas velocity component caused by the expansion and buoyancy of  the
             combustion product gases. Figure 4.7 illustratesthe experimentalrelationship among S,,
             S’,  and S, for spherical flame propagation in CH,  air as a function of equivalenceratio
             (fraction of stoichiometricfuel concentration).The maximum Sf  and S, values occur on
             the rich side of stoichiometriccomposition and the ratio S’/S,  is about 6. Under ideal adi-
             abatic conditions,the maximum S,/S,  ratio is about 7.5, which is typical of the combustion
             product expansion ratio E for most organic fuels. The plane, one-dimensional flame

















                                                  Figure 4.7   Flame speed Sfi gas  velocity  Sg:  and
                                                  burning velocity  S,  versus  equivalence  ratio  for
                                                  sphericalmethane/air flame propagation and atmo-
                                                  sphericpressure (From Kuchta, 1985;originallyfrom
                          EQUIVALENCE RATIO       Andrews and Bradley,  1972).
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