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A Study of the Effectiveness of a Narrow Channel Apparatus in Simulating Microgravity Flame Spread over Thin Fuels

机译:窄通道装置模拟稀薄燃料微重力火焰传播的有效性研究

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NASA's current flammability testing method for non-metallic solids is NASA-STD-(I)-6001A Test 1. Materials that allow for an upward flame propagation of six inches or more fail the flammability test. The flames in the Earth-based Test 1 are dominated by the upward-flowing buoyant gases, and this is not representative of actual flame behavior in microgravity, where there are no buoyant effects on flames. Scientists at NASA have shown that by spatially confining a horizontally spreading flame in the vertical direction, buoyant forces can be minimized in an Earth-based flame spread test. Results from flammability tests conducted in San Diego State University's Narrow Channel Apparatus (SDSU NCA) closely match results from NASA's Narrow Channel Apparatus at 1 atmosphere of pressure and 21% oxygen. The advantage of the SDSU NCA is that it not only minimizes buoyant effects, but it also allows flammability tests to be performed at normoxic equivalent atmospheres that more closely match future spacecraft cabin atmospheres. Normoxic conditions are achieved in the SDSU NCA by varying the total pressure, opposed flow oxidizer velocity, and oxygen concentration in the test channel. In our previous research we measured the flame spread rate across Whatman 44 ashless filter paper at total pressures from .27 to 1.0 atm and oxygen mole fractions from 0.77 to 0.21 respectively, along the normoxic curve for a gap height of 5 mm above and below the thin fuel. Significant differences in the flame spread rate were found, with much higher spread rates at the low pressure/high oxygen concentrations. This paper extends that work by comparing flame spread results from flammability tests conducted on Kimwipes* in the SDSU NCA and in true microgravity in NASA's Zero-Gravity Research Facility at several points along the normoxic curve. Also, a scaling analysis is conducted to study the effect of pressure on certain flame length scales.
机译:NASA当前用于非金属固体的可燃性测试方法是NASA-STD-(I)-6001A测试1。允许向上火焰传播六英寸或更多的材料未通过可燃性测试。地基测试1中的火焰主要由向上流动的浮力气体控制,这并不代表微重力下的实际火焰行为,因为微重力对火焰没有浮力影响。 NASA的科学家表明,通过在垂直方向上限制水平扩散的火焰,可以在基于地球的火焰扩散测试中将浮力最小化。在1个大气压和21%的氧气压力下,由圣地亚哥州立大学的窄通道仪器(SDSU NCA)进行的可燃性测试结果与NASA的窄通道仪器的结果非常吻合。 SDSU NCA的优点在于,它不仅使浮力效应最小化,而且还允许在与常年航天器机舱气氛更匹配的常氧当量气氛下进行可燃性测试。 SDSU NCA中的常氧条件是通过改变总压力,相反的流氧化剂速度和测试通道中的氧气浓度来实现的。在我们先前的研究中,我们沿着常氧曲线测量了在高空下和上下空出的间隙高度为5 mm时,Whatman 44无灰滤纸在总压力为.27至1.0 atm,氧气摩尔分数为0.77至0.21时的火焰蔓延率。稀薄的燃料。发现火焰蔓延速率存在显着差异,在低压/高氧气浓度下,火焰蔓延速率要高得多。本文通过比较在SDSU NCA中对Kimwipes *进行的可燃性测试的火焰扩散结果,以及在沿常氧曲线的几个点上对NASA零重力研究设施中的真实微重力进行的火焰扩散结果,扩展了这项工作。另外,进行了定标分析,以研究压力对某些火焰长度标度的影响。

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