Flow-Mach-number-variation-induced hysteresis in steady shock wave reflections

被引：29
|
作者：
Ivanov, MS [1 ]
Ben-Dor, G
Elperin, T
Kudryavtsev, AN
Khotyanovsky, DV
机构：
[1] Russian Acad Sci, Inst Theoret & Appl Mech, Computat Aerodynam Lab, Siberian Div, Novosibirsk 630090, Russia
[2] Ben Gurion Univ Negev, Dept Mech Engn, Pearlstone Ctr Aeronaut Engn Studies, IL-84105 Beer Sheva, Israel
来源：
AIAA JOURNAL | 2001年 / 39卷 / 05期
关键词：
D O I：
10.2514/2.1406
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Flow-mach-number-variation-induced hysteresis was studied in steady shock wave reflections. The flow between two symmetrically spaced wedges was simulated using a shock-capturing total variation diminishing (TVD) scheme. It was shown that a flow Mach number variation-induced hysteresis is possible in two-dimensional steady flows.
引用
收藏
页码：972 / 974
页数：3
相关论文
共 50 条
  • [41] Size and shape of shock waves and slip line for Mach reflection in steady flow
    Bai, Chen-Yuan
    Wu, Zi-Niu
    [J]. JOURNAL OF FLUID MECHANICS, 2017, 818 : 116 - 140
  • [42] Dynamic transition from Mach to regular reflection of shock waves in a steady flow
    Naidoo, K.
    Skews, B. W.
    [J]. JOURNAL OF FLUID MECHANICS, 2014, 750 : 385 - 400
  • [43] Stability and analogy of shock wave reflection in steady flow
    N. Sudani
    H.G. Hornung
    [J]. Shock Waves, 1998, 8 : 367 - 374
  • [44] Stability and analogy of shock wave reflection in steady flow
    Sudani, N
    Hornung, HG
    [J]. SHOCK WAVES, 1998, 8 (06) : 367 - 374
  • [45] Oscillation of the shock train under synchronous variation of incoming Mach number and backpressure
    Wang, Ziao
    Chang, Juntao
    Li, Yiming
    Chen, Ruoyu
    Hou, Wenxin
    Guo, Jifeng
    Yue, Lianjie
    [J]. PHYSICS OF FLUIDS, 2022, 34 (04)
  • [46] Numerical simulation of three-dimensional regular and Mach reflections of shock waves in steady flows
    Ivanov, MS
    Gimelshein, SF
    Kudryavtsev, AN
    Markelov, GN
    Khotyanovsky, DV
    [J]. COMPUTATIONAL FLUID DYNAMICS '98, VOL 1, PARTS 1 AND 2, 1998, : 869 - 874
  • [47] Sidewall influence of varying free stream Mach number in ramp induced shock wave boundary layer interactions
    Mangalagiri, Raja
    Jammy, Satya P.
    [J]. THEORETICAL AND APPLIED MECHANICS LETTERS, 2024, 14 (04)
  • [48] TRANSITION TO MACH REFLECTION OF SHOCK-WAVES IN STEADY AND PSEUDO-STEADY FLOW WITH AND WITHOUT RELAXATION
    HORNUNG, HG
    OERTEL, H
    SANDEMAN, RJ
    [J]. JOURNAL OF FLUID MECHANICS, 1979, 90 (FEB) : 541 - &
  • [49] STUDIES OF HIGH MACH NUMBER ([30) SHOCK WAVE PRODUCED BY PLASMA FOCUS
    NAKAGAWA, Y
    WISLER, DC
    [J]. BULLETIN OF THE AMERICAN PHYSICAL SOCIETY, 1969, 14 (11): : 1088 - &
  • [50] Detailed flow study of Mach number 1.6 high transonic flow with a shock wave in a pressure ratio 11 centrifugal compressor impeller
    Higashimori, H
    Hasagawa, K
    Sumida, K
    Suita, T
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2004, 126 (04): : 473 - 481
12345