By K. Ohtake (auth.), Professor Tsuneo Someya (eds.)
Non-uniform combustion, as encountered in diesel and gasoline turbine engines, furnaces, and boilers, is liable for the conversion of fossil gasoline to power and in addition for the corresponding formation of toxins. despite nice examine efforts some time past, the mechanism of non-uniform combustion has remained much less explored than that of different combustion varieties, because it comprises many, generally temporary approaches which effect one another. In view of this heritage, a gaggle study venture, "Exploration of Combustion Mechanism", used to be demonstrated to discover the mechanism of combustion, specially that of diffusive combustion, and likewise to discover effective how you can keep watch over the combustion strategy for larger usage of gasoline and the relief of pollutant emission. the crowd study was once begun, after preparatory job of two years, in April 1988, for a interval of three years, as a undertaking with a Grant-in-Aid for medical learn of precedence zone backed through the Ministry of schooling, technology and tradition of Japan. the whole team of forty three participants used to be organize as an organizing committee of thirteen individuals, and 5 study teams, which include 36 contributors. The examine teams have been: (1) regular combustion, (2) Unsteady spray combustion, (3) keep an eye on of combustion, (4) Chemistry of combustion, and (5) results of fuels. firstly of the undertaking it was once agreed that we must always pursue the mechanism of combustion from a systematic standpoint, specifically, the objective of the venture used to be to acquire the basics, or "know why", instead of "know how" of combustion.
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Extra info for Advanced Combustion Science
It is interesting to note that at this point the density decreases to zero almost discontinuously as we approach from the fuel side. On the other hand, the decrease is very gradual from the oxidizer side. The calculation predicts fairly well the general trend of the observation except one thing. It cannot predict the no particle region with a finite width as observed in the experiment. In Fig. 27 the predicted position of discontinuous decrease in the Colorimetric Analysis of Turbulent Flames 29 fuel side is plotted against the injection velocities as compared to the experimental observation.
2 5 0 VO o -5 -10 -15 -20 -15 Xc::) . 'I, -10 -5 0 1110 10 15 Fig. 2 temperature region is located below the jet axis. The formation of attached vortices is likely to result in the well-mixed region of the kidney shape in the wake of the flame where the chemical reaction proceeds very actively and consequently the flame temperature is rather high. It is also evident that the decrease in a velocity ratio makes the high temperature region move up to approach the axis of jet flame. 20 present the contours of isotherm, equi-concentration of CO, 02 and CO2 in terms of mole fraction in the transverse cross section at SID = 54.
26. The solid curves represent the calculated distribution as compared to the experimental distribution. The particle number density is made nondimensional by those at the nozzle exits. As is seen in the figure, the calculation predicts that there exists a point where the number density becomes zero. It is interesting to note that at this point the density decreases to zero almost discontinuously as we approach from the fuel side. On the other hand, the decrease is very gradual from the oxidizer side.