Effect of micro-ramps on supersonic boundary layer past a double wedge

被引：0
|
作者：
Zhang Qinghu
Xu Xiaobin
Wang Xiong
Lin Jingzhou
Tong Hua
机构：
[1] Hypervelocity Aerodynamics Institute of China Aerodynamics Research and Development Center,
来源：
Journal of Visualization | 2018年 / 21卷
关键词：
Flow visualization; Micro-ramp; Vortex structure; Double wedge;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1 / 4
页数：3
相关论文
共 50 条
  • [21] MHD BOUNDARY-LAYER FLOW PAST A MOVING WEDGE
    Ishak, A.
    Nazar, R.
    Pop, I.
    MAGNETOHYDRODYNAMICS, 2009, 45 (01): : 103 - 110
  • [22] Optimal disturbances in the supersonic boundary layer past a sharp cone
    Zuccher, Simone
    Shalaev, Ivan
    Tumin, Anatoli
    Reshotko, Eli
    AIAA JOURNAL, 2007, 45 (02) : 366 - 373
  • [23] UNIFIED UNSTEADY SUPERSONIC HYPERSONIC THEORY OF FLOW PAST DOUBLE WEDGE AIRFOILS
    HUI, WH
    ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND PHYSIK, 1983, 34 (04): : 458 - 488
  • [24] EXPERIMENTAL INVESTIGATION OF SUPERSONIC-FLOW PAST DOUBLE-WEDGE CONFIGURATIONS
    BERTIN, JJ
    HINKLE, JC
    AIAA JOURNAL, 1975, 13 (07) : 897 - 901
  • [25] ON BOUNDARY-LAYER FLOW OF A POWER LAW LIQUID PAST A WEDGE
    ROY, TR
    INDIAN JOURNAL OF PURE & APPLIED MATHEMATICS, 1980, 11 (11): : 1540 - 1547
  • [26] Mixed convection boundary layer flow past a wedge with permeable walls
    Leli Deswita
    Roslinda Nazar
    Anuar Ishak
    Rokiah Ahmad
    Ioan Pop
    Heat and Mass Transfer, 2010, 46 : 1013 - 1018
  • [27] Mixed convection boundary layer flow past a wedge with permeable walls
    Deswita, Leli
    Nazar, Roslinda
    Ishak, Anuar
    Ahmad, Rokiah
    Pop, Ioan
    HEAT AND MASS TRANSFER, 2010, 46 (8-9) : 1013 - 1018
  • [28] SUBSONIC AND SUPERSONIC BOUNDARY-LAYER FLOW PAST A WAVY WALL
    INGER, GR
    WILLIAMS, EP
    AIAA JOURNAL, 1972, 10 (05) : 636 - &
  • [29] Computation of hypersonic double wedge shock/boundary layer interaction
    Reinartz, B.
    Ballmann, J.
    SHOCK WAVES, VOL 2, PROCEEDINGS, 2009, : 1099 - 1104
  • [30] Mach reflection in steady supersonic flow considering wedge boundary-layer correction
    Zijun CHEN
    Chenyuan BAI
    Ziniu WU
    Chinese Journal of Aeronautics , 2020, (02) : 465 - 475
12345