SHOCK-BOUNDARY LAYER INTERACTION IN HYPERSONIC FLOW

被引：0
|
作者：
GAILLARD, L [1 ]
STORKMANN, V [1 ]
GRONIG, H [1 ]
机构：
[1] RHEIN WESTFAL TH AACHEN,STOSSWELLENLAB,D-52056 AACHEN,GERMANY
来源：
COMPTES RENDUS DE L ACADEMIE DES SCIENCES SERIE II FASCICULE B-MECANIQUE PHYSIQUE CHIMIE ASTRONOMIE | 1995年 / 321卷 / 05期
关键词：
D O I：
暂无
中图分类号：
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号：
07 ; 0710 ; 09 ;
摘要：
We study the hypersonic shock-flat plate boundary layer interaction. The boundary layer separation was detected. Its length is an increasing function of the Reynolds number at the interaction point (Re-X1). Downstream of the interaction, crossfluctuations of hat fluxes at the wall were observed; their amplitudes remain constant in terms of Re-X1; their average wavelength is invariant.
引用
收藏
页码：183 / 186
页数：4
相关论文
共 50 条
  • [21] NEW SHOCK DETECTOR AND IMPROVED CONTROL FUNCTION FOR SHOCK-BOUNDARY LAYER INTERACTION
    Liu, Chaoqun
    Fu, Huankun
    Lu, Ping
    INTERNATIONAL JOURNAL OF NUMERICAL ANALYSIS AND MODELING, 2012, 9 (02) : 276 - 288
  • [22] Thermal control of transonic shock-boundary layer interaction over a natural laminar flow airfoil
    Sengupta, Tapan K.
    Roy, Arkadyuti Ghosh
    Chakraborty, Ardhendu
    Sengupta, Aditi
    Sundaram, Prasannabalaji
    PHYSICS OF FLUIDS, 2021, 33 (12)
  • [23] Visualization of incipient flow separation condition on hypersonic shock–boundary layer interaction
    H. M. Talsaniya
    V. Menezes
    B. Nithin
    V. Kulkarni
    Journal of Visualization, 2015, 18 : 611 - 618
  • [24] EXPERIMENTS ON SHOCK-WAVE BOUNDARY-LAYER INTERACTION IN HYPERSONIC FLOW
    COET, MC
    CHANETZ, B
    RECHERCHE AEROSPATIALE, 1993, (01): : 61 - 74
  • [25] SHOCK WAVE-TURBULENT BOUNDARY-LAYER INTERACTION IN HYPERSONIC FLOW
    HOLDEN, MS
    ASTRONAUTICS & AERONAUTICS, 1977, 15 (10): : B7 - B7
  • [26] Direct numerical simulations of shock-boundary layer interaction at Ma=6
    Pagella, A
    Rist, U
    COMPUTATIONAL SCIENCE AND HIGH PERFORMANCE COMPUTING, 2005, 88 : 123 - 140
  • [27] Skin friction estimation on a surface under shock-boundary layer interaction
    Kshetrimayum, Maitri
    Irimpan, Kiran Joy
    Menezes, Viren
    SADHANA-ACADEMY PROCEEDINGS IN ENGINEERING SCIENCES, 2020, 45 (01):
  • [28] INVESTIGATIONS OF THE UNSTEADY SHOCK-BOUNDARY LAYER INTERACTION IN A TRANSONIC COMPRESSOR CASCADE
    Lopez, Edwin J. Munoz
    Hergt, Alexander
    Klinner, Joachim
    Grund, Sebastian
    Karboujian, Jirair
    Flamm, Jasmin
    Guemmer, Volker
    PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 13D, 2023,
  • [29] Porous Bleed Boundary Conditions for Supersonic Flows With & Without Shock-Boundary Layer Interaction
    Giehler, Julian
    Grenson, Pierre
    Bur, Reynald
    FLOW TURBULENCE AND COMBUSTION, 2023, 111 (04) : 1139 - 1173
  • [30] Skin friction estimation on a surface under shock-boundary layer interaction
    Maitri Kshetrimayum
    Kiran Joy Irimpan
    Viren Menezes
    Sādhanā, 2020, 45
12345