SERIES SOLUTIONS FOR SHOCK-TUBE LAMINAR BOUNDARY LAYER AND TEST TIME

被引：16

|

作者：

MIRELS, H

KING, WS

机构：

来源：

AIAA JOURNAL | 1966年 / 4卷 / 05期

关键词：

D O I：

10.2514/3.3547

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

收藏

页码：782 / &

相关论文

共 50 条

[1] LAMINAR BOUNDARY-LAYER AT VIBRATIONAL NONEQUILIBRIUM IN A SHOCK-TUBE
ZEITOUN, D
ACTA ASTRONAUTICA, 1975, 2 (9-10) : 879 - 889
[2] BOUNDARY-LAYER IN A SHOCK-TUBE
WALKER, JDA
DENNIS, SCR
JOURNAL OF FLUID MECHANICS, 1972, 56 (NOV14) : 19 - &
[3] SHOCK-TUBE CHEMISTRY .1. LAMINAR-TO-TURBULENT BOUNDARY-LAYER TRANSITION
BANDER, JA
SANZONE, G
JOURNAL OF PHYSICAL CHEMISTRY, 1977, 81 (01): : 1 - 3
[4] BOUNDARY-LAYER CLOSURE IN CONICAL SHOCK-TUBE
CONNOR, JG
PHYSICS OF FLUIDS, 1972, 15 (08) : 1403 - &
[5] INVESTIGATION OF THE SHOCK-TUBE BOUNDARY LAYER BY A TRACER METHOD
CHEN, CJ
EMRICH, RJ
PHYSICS OF FLUIDS, 1963, 6 (01) : 1 - 9
[6] SHOCK-TUBE STUDY OF BOUNDARY-LAYER INSTABILITY
BRUN, R
AUBERGER, P
VANQUE, N
ACTA ASTRONAUTICA, 1978, 5 (11-1) : 1145 - 1152
[7] INFLUENCE OF TURBULENT BOUNDARY LAYER ON SHOCK TUBE TEST TIME
JEANMARI.P
BROCHER, EF
AIAA JOURNAL, 1965, 3 (05) : 960 - &
[8] CORRELATION FORMULAS FOR LAMINAR SHOCK TUBE BOUNDARY LAYER
MIRELS, H
PHYSICS OF FLUIDS, 1966, 9 (07) : 1265 - &
[9] INFLUENCE OF REFLECTED SHOCK AND BOUNDARY-LAYER INTERACTION ON SHOCK-TUBE FLOWS
DAVIES, L
WILSON, JL
PHYSICS OF FLUIDS, 1969, 12 (5P2S) : I37 - &
[10] INTERACTION OF A REFLECTED SHOCK-WAVE WITH BOUNDARY-LAYER IN A SHOCK-TUBE
MATSUO, K
KAWAGOE, S
KAGE, K
BULLETIN OF THE JSME-JAPAN SOCIETY OF MECHANICAL ENGINEERS, 1974, 17 (110): : 1039 - 1046

← 1 2 3 4 5 →