Flow visualization of Mach 3 compression ramp with different upstream boundary layers
详细信息    查看全文
  • 作者:Yu Wu ; Shihe Yi ; Lin He ; Zhi Chen ; Yangzhu Zhu
  • 关键词:Compression ramp ; Boundary layer ; Flow visualization ; Fine flow structure
  • 刊名:Journal of Visualization
  • 出版年:2015
  • 出版时间:November 2015
  • 年:2015
  • 卷:18
  • 期:4
  • 页码:631-644
  • 全文大小:2,222 KB
  • 参考文献:Ardonceau PL (1984) The structure of turbulence in a supersonic shock-wave/boundary layer interaction. AIAA J 22(9):1254鈥?262CrossRef
    Bleilebens M, Olivier H (2006) On the influence of elevated surface temperatures on hypersonic shock wave boundary layer interaction at a heated ramp model. Shock Waves 15:301鈥?12CrossRef
    Bookey P, Wyckham C (2005) New experimental data of STBLI at DNS/LES accessible Reynolds numbers. AIAA Paper 2005-0309
    Chen Z, Yi S, He L, Zhu Y, Ge Y, Wu Y (2014) Spatial density fluctuation of supersonic flow over a backward-facing step measured by nano-tracer planar laser scattering. J Vis 17(4):345鈥?61CrossRef
    Disimile PJ, Scaggs NE (1989) An investigation into wedge induced turbulent boundary layer separation on a uniformly roughened surface at Mach 6. AIAA Paper 1989-2163
    Dolling D, Or C (1985) Unsteadiness of the shock wave structure in attached and separated compression ramp flows. Exp Fluids 3:24鈥?2CrossRef
    Ganapathisubramani B, Clemens N, Dolling D (2006) Planar imaging measurements to study the effect of spanwise structure of upstream turbulent boundary layer on shock induced separation. AIAA Paper 2006-0324
    Ganapathisubramani B, Clemens N, Dolling D (2009) Low-frequency dynamics of shock-induced separation in a compression ramp interaction. J Fluid Mech 636:397鈥?25MATH CrossRef
    Gang D, Yi S, Wu Y, Zhu Y (2014) Supersonic flow over circular protuberances on a flat plate. J Vis 17(4):307鈥?17CrossRef
    Holden M, Chadwick K (1995) Studies of laminar, transitional and turbulent hypersonic flows over curved compression surfaces. AIAA Paper 1995-0093
    Law CH (1975) Supersonic shock wave-turbulent boundary layer interactions. AIAA Paper 1975-0832
    Lee C, Wang S (1995) Study of the shock motion in a hypersonic shock system/turbulent boundary layer interaction. Exp Fluids 19:143鈥?49
    Lewis JE, Kubota T, Lees L (1967) Experimental investigation of supersonic laminar, two dimensional boundary layer separation in a compression corner with and without cooling. AIAA Paper 1967-0191
    Martin M, Smits A, Wu M, Ringuette M (2006) The turbulence structure of shockwave and boundary layer interaction in a compression corner. AIAA Paper 2006-0497
    Prince SA, Vannahme M, Stollery JL (1999) Experiments on the hypersonic turbulent shock-wave/boundary layer interaction and the effects of surface roughness. AIAA Paper 1999-0147
    Quan P, Yi S, Wu Y, Zhu Y, Chen Z (2014) Experimental investigation of interactions between laminar or turbulent boundary layer and shock wave. Acta Phys Sin 63(8):084703
    Ringuette M, Bookey P, Wyckham C, Smits A (2009) Experimental study of a Mach 3 compression ramp interaction at Re胃聽=聽2400. AIAA J 47:373鈥?85CrossRef
    Settles GS, Fitzpatrick TJ, Bogdonoff SM (1979) Detailed study of attached and separated compression corner flow fields in high Reynolds number supersonic flow. AIAA J 17(6):579鈥?85CrossRef
    Simeonides G, Haase W, Manna M (1994) Experimental, analytical and computational methods applied to hypersonic compression ramp flows. AIAA J 32(2):301鈥?10CrossRef
    Wu Y, Yi S, Chen Z, Zhang Q, Gang D (2013) Experimental investigations on structures of supersonic laminar/turbulent flow over a compression ramp. Acta Phys Sin 62(18):184702
    Yi S, He L, Zhao Y, Tian L, Cheng Z (2009) A flow control study of a supersonic mixing layer via NPLS. Sci China 52:2001鈥?006CrossRef
    Zhang Q, Yi S, Chen Z, Zhu Y, Zhou Y (2013) Visualization of supersonic flow over double wedge. J Vis 16:209鈥?17CrossRef
    Zhao Y, Yi S, Tian L, He L, Cheng Z (2009) Supersonic flow imaging via nanoparticles. Sci China 52:3640鈥?648MATH CrossRef
    Zhu Y, Yi S, He L, Tian L, Zhou Y (2013) Instantaneous and time-averaged flow structures around a blunt double-cone with or without supersonic film cooling visualized via nano-tracer planar laser scattering. Chin Phys B 22:014702CrossRef
  • 作者单位:Yu Wu (1)
    Shihe Yi (1)
    Lin He (1)
    Zhi Chen (1)
    Yangzhu Zhu (1)

    1. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, 410073, China
  • 刊物类别:Engineering
  • 刊物主题:Computer Imaging, Vision, Pattern Recognition and Graphics
    Engineering Fluid Dynamics
    Classical Continuum Physics
    Engineering Thermodynamics, Heat and Mass Transfer
  • 出版者:Springer Berlin / Heidelberg
  • ISSN:1875-8975
文摘

© 2004-2018 中国地质图书馆版权所有 京ICP备05064691号 京公网安备11010802017129号

地址:北京市海淀区学院路29号 邮编:100083

电话:办公室:(+86 10)66554848;文献借阅、咨询服务、科技查新:66554700