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Smoke-Point Properties of Non-Buoyant 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 non-buoyant round laminar jet diffusion flames were studied emphasizing results from long-duration (100-230 s) experiments at microgravity carried out in orbit aboard the space shuttle Columbia. Experimental conditions included ethylene- and propane-fueled flames burning in still air at an ambient temperature of 300 K, pressures of 35-130 kPa, jet exit diameters of 1.6 and 2.7 mm, jet exit velocities of 170-690 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. Contrary to the normal-gravity laminar smoke point, in microgravity, the onset of laminar smoke-point conditions involved two flame configurations: closed-tip flames with soot emissions along the flame axis and open-tip flames with 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 non-buoyant flames emitted soot more readily than non-buoyant flames in earlier tests using ground-based microgravity facilities and than buoyant flames at normal gravity, as a result of reduced effects of unsteadiness, flame disturbances, and buoyant motion. For example, present measurements of laminar smoke-point flame lengths at comparable conditions were up to 2.3 times shorter than ground-based microgravity measurements and up to 6.4 times shorter than buoyant flame measurements. Finally, present laminar smoke-point flame lengths were roughly inversely proportional to pressure to a degree that is a somewhat smaller than observed during earlier tests both at microgravity (using ground-based facilities) and at normal gravity.
机译:对非浮力圆形层流射流扩散火焰的层流烟点特性进行了研究,强调了哥伦比亚航天飞机在轨道上进行的微重力下的持续时间(100-230 s)实验的结果。实验条件包括以乙烯和丙烷为燃料的火焰在静止空气中在300 K的环境温度下燃烧,压力为35-130 kPa,射流出口直径为1.6和2.7 mm,射流出口速度为170-690 mm / s,射流雷诺数为46-172,特征性火焰停留时间为40-302 ms,发光长度为15-63 mm。与正常重力层流烟点相反,在微重力条件下,层流烟点条件的发作涉及两种火焰配置:沿火焰轴散发烟尘的密闭式火焰和来自环形环的烟尘散发的开放式火焰火焰轴。在大的特征性火焰停留时间观察到开尖火焰,同时出现了与靠近火焰尖端的辐射淬火相关的烟尘排放:尽管如此,仍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有很好的相关性。在不稳定性,火焰扰动和浮力运动的影响减小的结果下,目前的稳定和非浮力火焰在使用地面微重力设施的早期测试中比非浮力火焰更容易散发烟灰,并且比在正常重力下的浮力火焰更容易散发烟灰。例如,目前在可比较条件下对层状烟点火焰长度的测量比基于地面的微重力测量仪短2.3倍,比浮力火焰测量仪短6.4倍。最后,目前的层状烟点火焰长度大致与压力成反比,在某种程度上比早期试验在微重力(使用地面设施)和法向重力下所观察到的要小。

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