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

机译:窄通道装置在薄燃料上涂抹微匍匐火焰中的窄通道装置的有效性研究

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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:美国国家航空航天局的目前的非金属固体可燃性测试方法是NASA-STD-(I)-6001A试验1.允许向上火焰传播六英寸或更高的燃烧性试验的材料。基于地球测试1中的火焰由向上流动的浮力气体主导,这不是在微匍匐的情况下代表实际火焰行为,在那里对火焰没有浮力影响。美国宇航局的科学家表明,通过在垂直方向上空地限制水平扩散火焰,可以在基于地球的火焰传播测试中最小化浮力力。在圣地亚哥州立大学的窄通道装置(SDSU NCA)中进行的可燃性测试结果与NASA的窄沟道设备的结果紧密匹配,在1个压力和21%的氧气气氛中。 SDSU NCA的优点是它不仅最小化了浮力效应,而且还允许在常见匹配未来航天器舱室气氛的常见常见的等同气氛中进行易燃性测试。通过改变测试通道中的总压力,相反的流动氧化剂速度和氧浓度,在SDSU NCA中实现常氧条件。在我们以前的研究中,我们在从0.27至1.0 atm的总压力下,从0.27至1.0 atm和氧气级数的总压力下,沿常见曲线的间隙高度和下方的间隙高度分别为0.77至0.21,氧气摩尔分数的总压力分别测量了44个无灰滤纸。薄燃料。发现了火焰传播率的显着差异,低压/高氧浓度的扩展速率大得多。本文通过比较了在Kimwipes上进行的易燃性试验的火焰传播结果进行了比较了这种作品?在SDSU NCA和NASA在NASA的零重力研究设施中的真实微疱疹,沿常见氧化曲线的几点。而且,进行缩放分析以研究压力对某些火焰长度尺度的影响。

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