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Convective Burning for Specific Flow Conditions

The stagnant layer analysis offers a pedagogical framework for presenting the essence of diffusive burning. For the most part the one-dimensional stagnant layer approximated a two-dimensional boundary layer in which 6 = 5(x), with x the flow direction. For a convective boundary layer, the heat transfer coefficient, hc, is defined as [Pg.248]

This crude approximation allows us to extend the stagnant layer solution to a host of convective heat transfer counterpart burning problems. Recall that for Equations (9.41) and (9.42), we can write [Pg.248]

Thus we see that the reference temperature should have been Y(h[2c hc/(cpr) +TX, which is slightly different from Equation (9.56a). Nevertheless, we see that [Pg.248]

The blocking factor can alternatively be written from Equation (9.60) as [Pg.249]

To obtain approximate solutions for convection heating problems, we only need to identify a heat transfer problem that has a given theoretical or empirical correlation for hc. This is usually given in the form of the Nusselt number (Nu), [Pg.249]


See other pages where Convective Burning for Specific Flow Conditions is mentioned: [Pg.248]    [Pg.249]    [Pg.253]   


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