DEVELOPMENT OF A HIGH-PERFORMANCE CRYOGENIC SHOCK-TUBE

被引：7

作者：

CUMMINGS, JC ^{[1
]}

机构：

[1] CALTECH,GRAD AERONAUT LABS,PASADENA,CA

来源：

JOURNAL OF FLUID MECHANICS | 1974年 / 66卷 / OCT21期

关键词：

D O I：

10.1017/S0022112074000139

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

页码：177 / 187

页数：11

共 14 条

[1]

BENNETT FD, 1957, AERO ENG REV

[2]

CUMMINGS JC, 1973, THESIS CALIFORNIA I

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

GLASS, II ;

PATTERSON, GN .

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

[4]

GOODYER MJ, 1972, 7 AIAA AER TEST C PA

[5] CRYOGENIC SHOCK-TUBE [J].

LIEPMANN, HW ;

CUMMINGS, JC ;

RUPERT, VC .

PHYSICS OF FLUIDS, 1973, 16 (02) :332-333

[6] TEST TIME IN LOW-PRESSURE SHOCK TUBES [J].

MIRELS, H .

PHYSICS OF FLUIDS, 1963, 6 (09) :1201-1214

[7] SHOCK TUBE TEST TIME LIMITATION DUE TO TURBULENT-WALL BOUNDARY LAYER [J].

MIRELS, H .

AIAA JOURNAL, 1964, 2 (01) :84-93

[8] ON FLOW DURATION IN LOW-PRESSURE SHOCK TUBES [J].

ROSHKO, A .

PHYSICS OF FLUIDS, 1960, 3 (06) :835-842

[9]

RUPERT VC, 1972, THESIS CALIFORNIA I

[10] DEPENDENCE OF SHOCK-TUBE BOUNDARY LAYERS ON SHOCK STRENGTH [J].

STURTEVANT, B ;

OKAMURA, TT .

PHYSICS OF FLUIDS, 1969, 12 (08) :1723-+

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