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Jet Initiation of Deflagration and Detonation in Stoichiometric H_2-O_2-N_2 Mixtures

机译:化学计量比的H_2-O_2-N_2混合气的爆燃和爆轰射流引发

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摘要

New results are reported on the initiation of detonation in hydrogen-oxygen-nitrogen mixtures. These results were obtained at Caltech in the Hyjet facility which consists of an 1180-liter receiver vessel and a 28-liter driver vessel. Orifices of various diameters were used to connect the two vessels. The driver vessel is a 2.2-meterlong tube in which combustion is initiated at the end opposite to the connection to thee receiver vessel. A flame or detonation exits the driver vessel through the orifice and enters the receiver vessel, initiating combustion in the receiver vessel.ududPrevious work carried out in the Hyjet facility used a sensitive driver vessel mixture of 35.7% H_2, 17.9% O_2, and 46.4% N_2. Spark initiation of this mixture resulted in a detonation within the driver. The conditions under which a detonation would be initiated in the receiver vessel were measured as a function of the amount of dilution for stoichiometric hydrogen-oxygen-diluent mixtures in the receiver vessel.ududIn the present work, a less sensitive mixture of 20% H_2 and 80% air was used in the driver, resulting in a flame-jet entering into the receiver vessel instead of the detonation that was observed in previous tests. Critical amounts of nitrogen dilution in the receiver vessel were determined for three jet orifice diameters: 25, 64 and 92 mm and stoichiometric hydrogen-oxygen-nitrogen mixtures. the amount of diluent was measured using a parameter β equal to the molar ratio of N_2 to O_2. The critical value of beta required for prompt initiation of detonation was estimated from a series of experiments for each nozzle size. the critical value of β is estimated to be .4 for the 25-mm-diameter nozzle, 1.3 for the 64-mm-diameter nozzle, and 2.0 for the 92-mm-diameter nozzle. As expected, these values are substantially lower than those measured in the previous experiments that were conducted with the detonating driver mixture. In addition, the range of β for which secondary explosions (DDT) are observed in the present experiments is smaller than in the previous work in Hyjet with the detonating driver mixture.
机译:据报道,在氢-氧-氮混合物中引发爆炸的新结果。这些结果是在Hyjet工厂的Caltech公司获得的,该工厂由1180升的接收船和28升的驾驶船组成。使用各种直径的孔口连接两个容器。驱动容器是一个2.2米长的管,其中燃烧在与接收容器连接相反的一端开始。火焰或爆震通过孔口离开驱动容器并进入接收容器,从而在接收容器中开始燃烧。 ud ud在Hyjet设施中进行的先前工作使用的敏感驱动混合物为35.7%H_2、17.9%O_2,和46.4%N_2。该混合物的火花引发导致驾驶员内起爆。根据接收容器中化学计量的氢-氧-稀释剂混合物的稀释量来测量接收容器中引发爆炸的条件。 ud ud在本工作中,灵敏度较低的混合物为20驱动器中使用了%H_2和80%的空气,导致火焰射流进入接收容器,而不是先前测试中观察到的爆炸。对于三个喷射孔直径:25、64和92 mm,以及化学计量的氢-氧-氮混合物,确定接收容器中氮稀释的临界量。使用等于N_2与O_2的摩尔比的参数β来测量稀释剂的量。对于每种喷嘴尺寸,通过一系列实验估算了迅速起爆所需的β临界值。对于25毫米直径的喷嘴,β的临界值估计为.4,对于64毫米直径的喷嘴,β的临界值为1.3,对于92毫米直径的喷嘴,其临界值为2.0。正如预期的那样,这些值大大低于在使用爆炸起子混合物进行的先前实验中测得的值。另外,在本实验中观察到的二次爆炸(DDT)的β范围比在先有Hyjet的起爆驱动混合物中的β范围小。

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    Pfahl U. J.; Shepherd J. E.;

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  • 年度 1999
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