Visualization of conical vortex and shock in swept shock/turbulent boundary layer interaction flow

被引:10
作者
Sheng, Fa-jia [1 ]
Tan, Hui-jun [1 ]
Zhuang, Yi [1 ]
Huang, He-xia [1 ]
Chen, Hao [1 ]
Wang, Wei-xing [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing, Jiangsu, Peoples R China
关键词
WAVE;
D O I
10.1007/s12650-018-0512-4
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
Graphical abstract: [Figure not available: see fulltext.]. © 2018, The Visualization Society of Japan.
引用
收藏
页码:909 / 914
页数:6
相关论文
共 10 条
[1]   PHYSICAL MODEL OF THE SWEPT SHOCK-WAVE BOUNDARY-LAYER INTERACTION FLOWFIELD [J].
ALVI, FS ;
SETTLES, GS .
AIAA JOURNAL, 1992, 30 (09) :2252-2258
[2]  
Bolton JT, 2017, 20170985 AIAA
[3]  
Clifford CJ, 2017, 20171643 AIAA
[4]   Investigation of Three-Dimensional Shock Wave/Turbulent-Boundary-Layer Interaction Initiated by a Single Fin [J].
Fang, Jian ;
Yao, Yufeng ;
Zheltovodov, Alexandr A. ;
Lu, Lipeng .
AIAA JOURNAL, 2017, 55 (02) :509-523
[5]   Application of free interaction theory in swept shock wave/turbulent boundary layer interactions [J].
He, Gang ;
Zhou, Jin ;
Zhao, Yu-xin .
JOURNAL OF VISUALIZATION, 2018, 21 (02) :203-214
[6]  
Jones C, 2018, 20183705 AIAA
[7]   AN EXPERIMENTAL-STUDY OF THE INTERACTION BETWEEN A GLANCING SHOCK-WAVE AND A TURBULENT BOUNDARY-LAYER [J].
KUBOTA, H ;
STOLLERY, JL .
JOURNAL OF FLUID MECHANICS, 1982, 116 (MAR) :431-458
[8]   NUMERICAL INVESTIGATION OF THE HIGH-SPEED CONICAL FLOW PAST A SHARP FIN [J].
PANARAS, AG .
JOURNAL OF FLUID MECHANICS, 1992, 236 :607-633
[9]  
Token K.H., 1974, HEAT TRANSFER DUE SH
[10]   Supersonic flow imaging via nanoparticles [J].
Zhao YuXin ;
Yi ShiHe ;
Tian LiFeng ;
Cheng ZhongYu .
SCIENCE IN CHINA SERIES E-TECHNOLOGICAL SCIENCES, 2009, 52 (12) :3640-3648