SHOCK TUBE TECHNIQUE FOR STUDY OF AUTOIGNITION OF LIQUID FUEL SPRAYS

被引：14

作者：

MULLANEY, GJ

机构：

来源：

INDUSTRIAL AND ENGINEERING CHEMISTRY | 1958年 / 50卷 / 01期

关键词：

D O I：

10.1021/ie50577a032

中图分类号：

O69 [应用化学];

学科分类号：

081704 ;

摘要：

引用

页码：53 / 58

页数：6

共 9 条

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[2]

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[3]

GEIGER FW, 1949, M724 U MICH REPT

[4] A THEORETICAL AND EXPERIMENTAL STUDY OF SHOCK-TUBE FLOWS [J].

GLASS, II ;

PATTERSON, GN .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1955, 22 (02) :73-100

[5] ATTENUATION IN THE SHOCK TUBE .1. LAMINAR FLOW [J].

HOLLYER, RN .

[6]

HOLLYER RN, 1953, 7204 U MICH REPT, P122

[7]

JOST W, 1946, EXPLOSION COMBUSTION, P583

[8]

TRIMPI RL, 1955, TN3375 NATL ADV COMM

[9]

WAKIL MM, 1955, FUEL VAPORIZATION IG