Ignition of a combustible mixture by a hot unsteady gas jet

被引：6

作者：

Djebaili, N ^{[1
]}

Lisbet, R ^{[1
]}

Dupre, G ^{[1
]}

Paillard, C ^{[1
]}

机构：

[1] UNIV ORLEANS,ORLEANS,FRANCE

来源：

COMBUSTION SCIENCE AND TECHNOLOGY | 1995年 / 104卷 / 4-6期

关键词：

unsteady jet; hydrogen combustion; shock waves; hot jet; ignition limits;

D O I：

10.1080/00102209508907724

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

The study of the ignition of a combustible mixture induced by means of an unsteady gas jet, at an initial temperature ranging from 700 to 3000 K, requires the construction of an original test facility which consists of a shock tube connected to a combustion chamber via an injector. With this new experimental setup, the ignition conditions of hydrogen-air (+carbondioxide) mixtures, induced by a hot hydrogen-argon mixture, have been extensively studied, resulting in the determination of the ignition limits of these combustible mixtures, at an initial pressure and temperature of 100 kPa and 403 K respectively.

引用

页码：273 / 285

页数：13

共 13 条

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CONTI, RS ;

HERTZBERG, M .

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[8]

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[9]

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[10]

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