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Stretch rate effects and flame surface densities in premixed turbulent combustion up to 1.25 MPa

机译:高达1.25 MPa的预混湍流燃烧中的拉伸率效应和火焰表面密度

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Independent research at two centres using a burner and an explosion bomb has revealed important aspects of turbulent premixed flame structure. Measurements at pressures and temperatures up to 1.25 MPa and 673 K in the two rigs were aimed at quantifying the influences of flame stretch rate and strain rate Markstein number, Ma(sr), on both turbulent burning velocity and flame surface density. That on burning velocity is expressed through the stretch rate factor, I-0, or probability of burning, P-b(0.5). These depend on Ma(sr), but they grow in importance as the Karlovitz stretch factor, K, increases, and are evaluated from the associated burning velocity data. Planar laser tomography was employed to identify contours of reaction progress variable in both rigs. These enabled both an appropriate flame front for the measurement of the turbulent burning velocity to be identified, and flame surface densities, with the associated factors, to be evaluated. In the explosion measurements, these parameters were derived also from the flame surface area, the derived P-b(0.5) factor and the measured turbulent burning velocities. In the burner measurement they were calculated directly from the flame surface density, which was derived from the flame contours.
机译:在两个使用燃烧器和爆炸弹的中心进行的独立研究发现了湍流预混火焰结构的重要方面。在这两个装置中,在高达1.25 MPa和673 K的压力和温度下进行测量旨在量化火焰拉伸速率和应变速率Markstein数Ma(sr)对湍流燃烧速度和火焰表面密度的影响。通过拉伸速率因子I-0或燃烧概率P-b(0.5)表示燃烧速度。它们取决于Ma(sr),但是随着Karlovitz拉伸因子K的增加,它们的重要性就越来越高,并且可以根据相关的燃烧速度数据进行评估。平面激光层析成像技术可用于识别两个钻机中反应进度变量的轮廓。这些使得既可以识别用于测量湍流燃烧速度的合适火焰前沿,也可以评估具有相关因素的火焰表面密度。在爆炸测量中,这些参数还来自火焰表面积,派生的P-b(0.5)因子和测得的湍流燃烧速度。在燃烧器测量中,它们是直接从火焰轮廓得出的火焰表面密度计算得出的。

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