Operation of the ISL transonic shock tube in a high subsonic flow regime

被引：0

|

作者：

Seiler, F ^{[1
]}

Havermann, M ^{[1
]}

Boller, F ^{[1
]}

Mangold, P ^{[1
]}

Takayama, K ^{[1
]}

机构：

[1] French German Res Inst St Louis, Shock Tube Dept, F-68301 St Louis, France

来源：

Shock Waves, Vols 1 and 2, Proceedings | 2005年

关键词：

D O I：

10.1007/978-3-540-27009-6_44

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

收藏

页码：307 / 312

页数：6

相关论文

共 50 条

[31] COMPUTATION OF SUBSONIC AND TRANSONIC HELICOPTER ROTOR FLOW USING EULER EQUATIONS
KRAMER, E
HERTEL, J
WAGNER, S
[J]. VERTICA, 1988, 12 (03): : 279 - 291
[32] COMPUTATION OF SUBSONIC VISCOUS AND TRANSONIC VISCOUS INVISCID UNSTEADY-FLOW
MULLER, UR
HENKE, H
[J]. COMPUTERS & FLUIDS, 1993, 22 (4-5) : 649 - 661
[33] 3-DIMENSIONAL COMPOSITE VELOCITY SOLUTIONS FOR SUBSONIC TRANSONIC FLOW
GORDNIER, RE
RUBIN, SG
[J]. AIAA JOURNAL, 1991, 29 (05) : 750 - 757
[34] LOSSES IN SUBSONIC AND TRANSONIC AXIAL-FLOW COMPRESSORS AT OPTIMUM CONDITIONS
PROVENZALE, GE
[J]. JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (05): : 431 - 432
[35] HIGH SUBSONIC FLOW WITH NORMAL SHOCK WAVE AT NEARLY CRITICAL MACH NUMBER
SAKURAI, T
[J]. JOURNAL OF THE PHYSICAL SOCIETY OF JAPAN, 1959, 14 (05) : 658 - 663
[36] TRANSITION REGIME TUBE FLOW
MARCHMAN, JF
MASON, WH
[J]. MECHANICAL ENGINEERING, 1972, 94 (06) : 59 - &
[37] APPROXIMATE TRANSONIC PROFILE FLOW AT INCIDENCE WITH SHOCK
NIYOGI, P
SEN, R
[J]. ACTA MECHANICA, 1978, 30 (1-2) : 65 - 77
[38] Transonic Gas Flow with Nonplanar Shock Waves
Kazakova M.Y.
[J]. Journal of Mathematical Sciences, 2014, 203 (4) : 499 - 508
[39] Compressible Flow and Transonic Shock in a Diverging Nozzle
Shuxing Chen
[J]. Communications in Mathematical Physics, 2009, 289 : 75 - 106
[40] Compressible Flow and Transonic Shock in a Diverging Nozzle
Chen, Shuxing
[J]. COMMUNICATIONS IN MATHEMATICAL PHYSICS, 2009, 289 (01) : 75 - 106

← 1 2 3 4 5 →