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The occurrence of the maximum peak overpressure mainly depended on the maximum flame surface area within the duct.
The flame surface density is in agreement with the aforementioned flame front curvature PDFs in that increasing the pressure and hydrogen concentration leads to an increase in the maximum flame surface density.
The maximum flame surface density tends to show linear dependence on the K-factor given as a function of the integral length scale and u′0/SL.
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Specifically, with increasing the turbulence intensity, the mean-progress-variable at which the flame surface density features a maximum decreases from values greater than 0.5 to values smaller than 0.5.
The maximum flame temperature did not change as a function of position along the curved flame surface, suggesting that the local agent concentration required for suppression will not differ significantly along the flame sheet.
Open image in new window Fig. 6 Maximum flame length and speeds for baseline (test 2) and active barrier tests.
Open image in new window Fig. 7 Maximum flame length and speeds for baseline (average test 1 and 7) and active barrier tests.
The maximum flame temperature was measured by a compensated thermocouple on the flame tip.
The maximum flame temperature, however, remains constant.
Capacity to operate with a minimum amount of excess air (maximum flame temperature).
But further augmentation in the sweep flow rates reduces the maximum flame temperature obtained.
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