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Laminar burning velocities of lean hydrogen-air mixtures at pressures up to 1.0 MPa

机译:贫氢空气混合物在高达1.0 MPa的压力下的层流燃烧速度

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Values of laminar burning velocity, u_1, and the associated strain rate Markstein number, Ma_(sr), of H_2-air mixtures have been obtained from measurements of flame speeds in a spherical explosion bomb with central ignition. Pressures ranged from 0.1 to 1.0 MPa, with values of equivalence ratio between 0.3 and 1.0. Many of the flames soon became unstable, with an accelerating flame speed, due to Darrieus-Landau and thermodiffusive instabilities. This effect increased with pressure. The flame wrinkling arising from the instabilities enhanced the flame speed. A method is described for allowing for this effect, based on measurements of the flame radii at which the instabilities increased the flame speed. This enabled u_1 and Ma_(sr) to be obtained, devoid of the effects of instabilities. With increasing pressure, the time interval between the end of the ignition spark and the onset of flame instability, during which stable stretched flame propagation occurred, became increasingly small and very high camera speeds were necessary for accurate measurement. Eventually this time interval became so short that first Ma_(sr) and then u_1 could not be measured. Such flame instabilities throw into question the utility of u_1 for high pressure, very unstable, flames. The measured values of u_1 are compared with those predicted by detailed chemical kinetic models of one-dimensional flames.
机译:H_2-空气混合物的层流燃烧速度u_1和相关应变率马克斯坦数Ma_(sr)的值已通过在带有中心点火的球形爆炸弹中的火焰速度测量中获得。压力范围为0.1到1.0 MPa,当量比的值在0.3到1.0之间。由于Darrieus-Landau和热扩散的不稳定性,许多火焰很快变得不稳定,火焰速度加快。该作用随压力增加。由不稳定性引起的火焰起皱提高了火焰速度。描述了一种方法,该方法基于不稳定性增加了火焰速度的火焰半径的测量来允许这种效果。这使得u_1和Ma_(sr)得以获得,而没有不稳定的影响。随着压力的增加,点火火花的结束与火焰不稳定性开始之间的时间间隔变得越来越小,在此期间发生稳定的拉伸火焰传播的时间间隔变得越来越小,因此需要非常高的相机速度才能进行精确测量。最终,这个时间间隔变得如此之短,以至于无法测量首先的Ma_(sr),然后无法测量u_1。这种火焰不稳定性使u_1在高压,非常不稳定的火焰中的效用受到质疑。将u_1的测量值与一维火焰的详细化学动力学模型预测的值进行比较。

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