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

页码：307 / 312

页数：6

共 50 条

[41] FLOW OVER A HELICOPTER BLADE TIP IN TRANSONIC REGIME
CARADONNA, FX
PHILIPPE, JJ
[J]. VERTICA, 1978, 2 (01): : 43 - 60
[42] A SHOCK INDICATOR FOR ADAPTIVE TRANSONIC FLOW COMPUTATIONS
GOHNER, U
WARNECKE, G
[J]. NUMERISCHE MATHEMATIK, 1994, 66 (04) : 423 - 448
[43] Control of the Flow over a Delta Wing in the Transonic Regime
Riou, Jacques
Garnier, Eric
Basdevant, Claude
[J]. AIAA JOURNAL, 2010, 48 (08) : 1851 - 1855
[44] A computational technique for high enthalpy shock tube and shock tunnel flow simulation
Sheng, Y
Sislian, JP
Liu, JJ
[J]. SHOCK WAVES, 1998, 8 (04) : 203 - 214
[45] A computational technique for high enthalpy shock tube and shock tunnel flow simulation
Y. Sheng
J.P. Sislian
J.J. Liu
[J]. Shock Waves, 1998, 8 : 203 - 214
[46] SUBSONIC AND TRANSONIC FLOW FIELD IN TWO-DIMENSIONAL DE LAVAL NOZZLES
Pu Qun Lin Tongji (Lin
[J]. Acta Mechanica Sinica, 1985, (01) : 1 - 8
[47] An inverse blade design method for subsonic and transonic viscous flow in compressors and turbines
Daneshkhah, K
Ghaly, WS
[J]. INVERSE PROBLEMS IN SCIENCE AND ENGINEERING, 2006, 14 (03) : 211 - 231
[48] AERODYNAMIC CHARACTERISTICS OF A TWO-DIMENSIONAL MOVING SPOILER IN SUBSONIC AND TRANSONIC FLOW
CONSIGNY, H
GRAVELLE, A
MOLINARO, R
[J]. JOURNAL OF AIRCRAFT, 1984, 21 (09): : 687 - 693
[49] Subsonic impulsively starting flow at a high angle of attack with shock wave and vortex interaction
Bai, Chenyuan
Li, Juan
Wu, Ziniu
[J]. CHINESE JOURNAL OF AERONAUTICS, 2018, 31 (09) : 1822 - 1828
[50] Subsonic impulsively starting flow at a high angle of attack with shock wave and vortex interaction
Chenyuan BAI
Juan LI
Ziniu WU
[J]. Chinese Journal of Aeronautics, 2018, (09) : 1822 - 1828

← 1 2 3 4 5 →