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Extra info for Aircraft Performance & Design
The measured velocity profile deviates from the dot-dash line with a further decrease in y. 2 compared velocity profiles measured with aluminum particles and with silicone oil droplets and showed that the point where the velocity profile starts to deviate from the straight velocity profile corresponds to the location of the upstream end of the flame wrinkling. With a further decrease in y, the data rate of velocity measurement decreased. In this region, the flame zone crosses the measured volume and the data are taken only when the measured volume is located on the unburnt side.
747-754. 9 Abdel Gayed, R. G. S. , 1977, pp. 17251735. 10 Cheng, R. K, and Ng, T. , "Velocity Statistics in Premixed Turbulent Flames," Combustion and Flame, Vol. 52, 1983, pp. 185202. , Law, C. , and Wu, C. K, "Laminar Flame Speeds of Hydrocarbon and Air Mixture with Hydrogen Addition," Combustion and Flame, Vol. 86, 1986, pp. 337-347. 12 Kim, Y. , "Propagation and Extinction of a Flame in a Stagnation-Point Flow," Combustion and Flame, Vol. 73, 1988, pp. 303-313. Near-Field CARS Measurements and the Local Extinction of TYirbulent Jet Diffusion Flames Fumiaki Takahashi* and Marlin D.
6"8 This is due to the fact that the flame front corrugations will burn themselves out faster than before, and higher levels of interface perturbation will be required to achieve the same deformation of the flame front. This is verified in the series of photographs presented in Fig. 7. Again, the initial stage of the interaction (up to t = 400 /^s) is similar to the other shots. Note that after the reflected shock has passed through the deformed flame, the scale of corrugations is not as fine as before (compare with Fig.