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Backdraft phenomena.

机译:反流现象。

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摘要

The purpose of this project was to develop a fundamental physical understanding of backdraft phenomena. The research was divided into three phases: exploratory simulations, gravity current modeling, and quantitative backdraft experiments. The primary goal of the first phase was to safely simulate a backdraft in the laboratory. A half-residential-scale compartment was built to conduct exploratory experiments. The initial experiments concluded with a scenario describing the fundamental physics of backdrafts. The importance of the gravity current which enters the compartment after opening was identified. In the second phase, the gravity current speed and the extent of its mixed region was investigated in a series of scaled salt water experiments. The scaled compartment (0.3m x 0.15m x 0.15m) was fitted with a variety of end openings: full, slot, door, and window. Video and photo data indicate that the mixing layer which rides on the gravity current in the full opening case, expands to occupy nearly the entire current in the partial opening cases. The Froude number and nondimensional head height are independent of {dollar}beta{dollar} and are in good agreement with numerical simulations and special limits from the literature.; In the final phase, 28 backdraft experiments were conducted in a 1.2 m by 1.2 m by 2.4 m compartment. A methane burner was ignited inside a closed compartment and allowed to burn as long as oxygen was available. After the flame extinguished due to oxygen starvation, the burner was left on to allow the unburned fuel fraction to increase. Upon opening the hatch a gravity current enters the compartment and travels across the floor to the ignition source. After ignition a deflagration rips through the compartment and out the opening culminating in a large fireball. Histories recorded included: fuel flow rates, upper layer temperatures, lower layer temperatures, opening velocities, compartment pressures, upper layer species concentrations for O{dollar}sb2,{dollar} CO{dollar}sb2,{dollar} CO, and HC. Results indicate that unburned fuel mass fractions {dollar}>{dollar}15% are necessary for a backdraft to occur and that the backdraft severity strongly depends on the delay time and species concentrations.
机译:该项目的目的是发展对回潮现象的基本物理理解。研究分为三个阶段:探索性模拟,重力流建模和定量反演实验。第一阶段的主要目标是在实验室中安全地模拟反向气流。建立了一个半住宅规模的隔间以进行探索性实验。最初的实验以描述反向草稿的基本物理原理的方案结束。确定了打开后进入舱室的重力流的重要性。在第二阶段,通过一系列规模化盐水实验研究了重力流速度及其混合区域的范围。可缩放的隔间(0.3m x 0.15m x 0.15m)配有各种端部开口:完整,开槽,门和窗户。视频和照片数据表明,在完全打开的情况下,依靠重力流流动的混合层在部分打开的情况下扩展以占据几乎全部电流。 Froude数和无量纲的头部高度与{dollar} beta {dollar}无关,并且与数值模拟和文献中的特殊限制非常吻合。在最后阶段,在1.2 m x 1.2 m x 2.4 m的隔室中进行了28次反草案实验。甲烷燃烧器在密闭室内点燃,只要有氧气就可以燃烧。火焰由于氧气不足而熄灭后,将燃烧器置于打开状态,以增加未燃烧的燃料份额。打开舱门时,重力流进入车厢,并穿过地板到达点火源。点火后,爆燃会穿过车厢,并从开口处喷出,最终形成大火球。记录的历史记录包括:燃料流量,上层温度,下层温度,打开速度,隔室压力,O {dollarssb2,{dollar} CO {dollar} sb2,{dollar} CO和HC的上层物质浓度。结果表明,未燃燃料质量分数{dollar}> {dollar} 15%对于发生反吹是必要的,并且反吹的严重性在很大程度上取决于延迟时间和物质浓度。

著录项

  • 作者单位

    University of California, Berkeley.;

  • 授予单位 University of California, Berkeley.;
  • 学科 Engineering Civil.; Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1993
  • 页码 235 p.
  • 总页数 235
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 建筑科学;机械、仪表工业;
  • 关键词

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