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Smoke-Point Properties of Nonbuoyant Round Laminar Jet Diffusion Flames

机译:非浮力圆形层流射流扩散火焰的烟点特性

摘要

The laminar smoke-point properties of nonbuoyant round laminar jet diffusion flames were studied emphasizing results from long duration (100-230 s) experiments at microgravity carried -out on- orbit in the Space Shuttle Columbia. Experimental conditions included ethylene-and propane-fueled flames burning in still air at an ambient temperature of 300 K, initial jet exit diameters of 1.6 and 2.7 mm, jet exit velocities of 170-1630 mm/s, jet exit Reynolds numbers of 46-172, characteristic flame residence times of 40-302 ms, and luminous flame lengths of 15-63 mm. The onset of laminar smoke-point conditions involved two flame configurations: closed-tip flames with first soot emissions along the flame axis and open-tip flames with first soot emissions from an annular ring about the flame axis. Open-tip flames were observed at large characteristic flame residence times with the onset of soot emissions associated with radiative quenching near the flame tip; nevertheless, unified correlations of laminar smoke-point properties were obtained that included both flame configurations. Flame lengths at laminar smoke-point conditions were well-correlated in terms of a corrected fuel flow rate suggested by a simplified analysis of flame shape. The present steady and nonbuoyant flames emitted soot more readily than earlier tests of nonbuoyant flames at microgravity using ground-based facilities and of buoyant flames at normal gravity due to reduced effects of unsteadiness, flame disturbances and buoyant motion. For example, laminar smoke-point flame lengths from ground-based microgravity measurements were up to 2.3 times longer and from buoyant flame measurements were up to 6.4 times longer than the present measurements at comparable conditions. Finally, present laminar smoke-point flame lengths were roughly inversely proportional to pressure, which is a somewhat slower variation than observed during earlier tests both at microgravity using ground-based facilities and at normal gravity.
机译:研究了非浮力圆形层流射流扩散火焰的层流烟点特性,强调了哥伦比亚航天飞机在轨进行的微重力下长时间(100-230 s)实验的结果。实验条件包括在环境温度为300 K的静止空气中燃烧的以乙烯和丙烷为燃料的火焰,初始射流出口直径为1.6和2.7 mm,射流出口速度为170-1630 mm / s,射流雷诺数为46- 172,特征火焰停留时间为40-302 ms,发光火焰长度为15-63 mm。层流烟点条件的发作涉及两种火焰配置:沿火焰轴具有第一烟尘排放的密闭式火焰和来自围绕火焰轴的环形环具有第一烟尘排放的开尖式火焰。在较大的特征火焰停留时间观察到了开尖火焰,并且出现了与靠近火焰尖端的辐射淬火相关的烟尘排放。然而,获得了包括两个火焰构型的层状烟点特性的统一相关性。层流烟点条件下的火焰长度与通过对火焰形状的简化分析所建议的校正后的燃料流量密切相关。与使用地面设施的微重力非浮力火焰和正常重力下的浮力火焰的早期测试相比,当前的稳定和非浮力火焰更容易散发烟灰,这是由于不稳定,火焰扰动和浮力运动的影响减小。例如,在可比较的条件下,基于地面的微重力测量得出的层状烟点火焰长度比当前测量长2.3倍,而根据浮力火焰测量得出的层烟点火焰长则比当前测量长6.4倍。最后,目前的层状烟点火焰长度大致与压力成反比,与使用地面设施在微重力下和在正常重力下进行的早期测试中观察到的变化相比,其变化速度稍慢。

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