SHOCK-FRONT-THICKNESS MEASUREMENTS BY AN ELECTRON BEAM TECHNIQUE

被引：24
作者：
BALLARD, HN
VENABLE, D
机构：
来源：
PHYSICS OF FLUIDS | 1958年 / 1卷 / 03期
关键词：
D O I：
10.1063/1.1724346
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
引用
收藏
页码：225 / 229
页数：5
相关论文
共 16 条
[1]  
Becker R., 1922, Z PHYS, V8, P321, DOI DOI 10.1007/BF01329605
[2]  
BURNETT D, 1935, P LOND MATH SOC, V40, P382, DOI DOI 10.1112/PLMS/S2-40.1.382
[3]   THE EXPERIMENTAL DETERMINATION OF THE THICKNESS OF A SHOCK FRONT IN A GAS [J].
COWAN, GR ;
HORNIG, DF .
JOURNAL OF CHEMICAL PHYSICS, 1950, 18 (08) :1008-1018
[4]  
GILBARG D, 1953, J RATION MECH ANAL, V2, P617
[5]   THE PROFILE OF A STEADY PLANE SHOCK WAVE [J].
GRAD, H .
COMMUNICATIONS ON PURE AND APPLIED MATHEMATICS, 1952, 5 (03) :257-300
[6]  
GREENE, 1951, J CHEM PHYS, V19, P427
[7]  
KAPLAN DE, 1955, J APPL PHYS, V26, P639
[8]   ON A COMPLETE SOLUTION OF THE ONE-DIMENSIONAL FLOW EQUATIONS OF A VISCOUS, HEAT-CONDUCTING, COMPRESSIBLE GAS [J].
MORDUCHOW, M ;
LIBBY, PA .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (11) :674-&
[9]  
MOTTSMITH HM, 1951, PHYS REV, V83, P885
[10]  
Rayleigh, 1910, P R SOC LOND A-CONTA, V84, P247
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