Dossier: LES4ICE'16: LES for Internal Combustion Engine Flows Conference
Open Access

Figure 8


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(a) Examples of measured and simulated 2D projected flame kernel area. A single-cycle example of the burned-gas area evolution for a measured cycle is used to quantify the laminar-turbulent transition time, τlam-turb, shown by the red-diamond in (b), which occurs much earlier than the 1% MBF from the AHR analysis (c).

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