The regular reflection→Mach reflection transition in unsteady flow over convex surfaces

被引:16
|
作者
Geva, M. [1 ]
Ram, O. [1 ]
Sadot, O. [1 ]
机构
[1] Ben Gurion Univ Negev, Fac Engn Sci, Dept Mech Engn, Pearlstone Ctr Aeronaut Engn Studies, IL-84105 Beer Sheva, Israel
基金
以色列科学基金会;
关键词
compressible flows; shock waves; SHOCK-WAVE REFLECTION; MACH REFLECTION; STEADY;
D O I
10.1017/jfm.2017.835
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The non-stationary transition from regular reflection (RR) to Mach reflection (MR) over convex segments has been the focus of many recent studies. Until recently, the problem was thought to be very complicated because it was believed that many parameters such as the radius of curvature, initial angle and geometrical shape of the reflecting surface influenced this process. In this study, experiments and inviscid numerical computations were performed in air (gamma = 1.4) at an incident shock-wave Mach number of 1.3. The incident shock waves were reflected over cylindrical and elliptical convex surfaces. The computations were validated by high-resolution experiments, which enabled the detection of features in the flow having characteristic lengths as small as 0.06 mm. Therefore, the RR -> MR transition and Mach stem growth were successfully validated in the early stages of the Mach stem formation and closer to the surface than ever before. The evolution of the RR, the transition to MR and the Mach stem growth were found to depend only on the radius of the reflecting surface. The reflected shock wave adjusts itself to the changing angles of the reflecting surface. This feature, which was demonstrated at Mach numbers 1.3 and 1.5, distinguishes the unsteady case from the self-similar pseudo-steady case and requires the formulation of the conservation equations. A modification of the standard two-shock theory (2ST) is presented to predict the flow properties behind a shock wave that propagates over convex surfaces. Until recently, the determination of the time-dependent flow properties was possible solely by numerical computations. Moreover, this derivation explains the controversial issue on the delay in the transition from the RR to the MR that was observed by many researchers. It turns out that the entire RR evolution and the particular moment of transition to MR, are based on the essential 'no-penetration' condition of the flow. Therefore, we proposed a simple geometrical criterion for the RR -> MR transition.
引用
收藏
页码:48 / 79
页数:32
相关论文
共 50 条
  • [31] EXPERIMENTS ON TRANSITION OF MACH REFLECTION
    HENDERSON, LF
    LOZZI, A
    JOURNAL OF FLUID MECHANICS, 1975, 68 (MAR11) : 139 - 155
  • [32] Downstream pressure induced hysteresis in the regular<->Mach reflection transition in steady flows
    BenDor, G
    Elperin, T
    Li, H
    Vasiliev, E
    PHYSICS OF FLUIDS, 1997, 9 (10) : 3096 - 3098
  • [33] Dynamic effects in transition from regular to Mach reflection in steady supersonic flows
    Goyal, Rohtash
    Sameen, A.
    Jayachandran, T.
    Rajesh, G.
    PHYSICAL REVIEW E, 2021, 104 (05)
  • [34] Numerical confirmation of the hysteresis phenomenon in the regular to the Mach reflection transition in steady flows
    Chpoun, A
    BenDor, G
    SHOCK WAVES, 1995, 5 (04) : 199 - 203
  • [35] REGULAR AND MACH REFLECTION OF SHOCK-WAVES
    HORNUNG, H
    ANNUAL REVIEW OF FLUID MECHANICS, 1986, 18 : 33 - 58
  • [36] A simple physical theory of weak Mach reflection over plane surfaces
    R.J. Sandeman
    Shock Waves, 2000, 10 : 103 - 112
  • [37] TRANSITION FROM REGULAR TO MACH REFLECTION OF SHOCK-WAVES .2. THE STEADY-FLOW CRITERION
    HORNUNG, HG
    ROBINSON, ML
    JOURNAL OF FLUID MECHANICS, 1982, 123 (OCT) : 155 - 164
  • [38] INVESTIGATIONS OF MACH REFLECTION OF A SHOCK-WAVE .4. THE TRANSITION BETWEEN REGULAR AND MACH REFLECTIONS
    MATSUO, K
    AOKI, T
    HIRAHARA, H
    KONDOH, N
    KISHIGAMI, T
    BULLETIN OF THE JSME-JAPAN SOCIETY OF MECHANICAL ENGINEERS, 1986, 29 (248): : 434 - 438
  • [39] FURTHER EXPERIMENTS ON TRANSITION TO MACH REFLECTION
    HENDERSON, LF
    LOZZI, A
    JOURNAL OF FLUID MECHANICS, 1979, 94 (OCT) : 541 - &
  • [40] Symmetric Mach reflection configuration with asymmetric unsteady solution
    Chenyuan BAI
    Miaomiao WANG
    Ziniu WU
    Chinese Journal of Aeronautics , 2023, (04) : 75 - 78