Microramp control of supersonic oblique shock-wave/boundary-layer interactions

被引：0
|
作者：
Babinsky, H. [1 ,2 ]
Li, Y. [1 ,2 ]
Ford, C.W. Pitt [1 ,2 ]
机构：
[1] Cambridge University, Cambridge, CB2 1PZ, United Kingdom
[2] Department of Engineering, United Kingdom
来源：
AIAA Journal | 2009年 / 47卷 / 03期
关键词：
Flow separation;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Journal article (JA)
引用
收藏
页码：668 / 675
相关论文
共 39 条
  • [1] Shock-Wave/Boundary-Layer Interactions in Transitional Rectangular Duct Flows
    David J. Lusher
    Neil D. Sandham
    Flow, Turbulence and Combustion, 2020, 105 : 649 - 670
  • [2] Shock-Wave/Boundary-Layer Interactions in Transitional Rectangular Duct Flows
    Lusher, David J.
    Sandham, Neil D.
    FLOW TURBULENCE AND COMBUSTION, 2020, 105 (02) : 649 - 670
  • [3] Effects of herringbone riblets on shock-wave/turbulent boundary-layer interactions
    Wen, Bo
    Zhong, Shan
    Wang, Gang
    Li, Lin
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 146
  • [4] Vortex Generators for Corner Separation Caused by Shock-Wave/Boundary-Layer Interactions
    Koike, Shunsuke
    Babinsky, Holger
    JOURNAL OF AIRCRAFT, 2019, 56 (01): : 239 - 249
  • [5] Control of shock-wave/boundary-layer interaction using abackward-facing step
    Zhai, Jian
    Zhang, Chen-An
    Wang, Fa-Min
    Zhang, Wei-Wei
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 126
  • [6] Effects of Number of Bleed Holes on Shock-Wave/Boundary-Layer Interactions in a Transonic Compressor Stator
    Li, Bai
    Zhou, Xun
    Luo, Lei
    Du, Wei
    JOURNAL OF THERMAL SCIENCE, 2024, 33 (02) : 611 - 624
  • [7] A Numerical Investigation on the Equivalence of Shock-Wave/Boundary-Layer Interactions using a Two Equations RANS Model
    John, B.
    Vivekkumar, P.
    JOURNAL OF APPLIED FLUID MECHANICS, 2021, 14 (03) : 753 - 767
  • [8] Flow control technique for shock wave/turbulent boundary layer interactions
    Shi X.
    Lyu M.
    Zhao Y.
    Tao S.
    Hao L.
    Yuan X.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2022, 43 (01):
  • [9] Control of shock-wave boundary layer interaction using steady micro-jets
    Verma, S. B.
    Manisankar, C.
    Akshara, P.
    SHOCK WAVES, 2015, 25 (05) : 535 - 543
  • [10] Control of shock-wave boundary layer interaction using steady micro-jets
    S. B. Verma
    C. Manisankar
    P. Akshara
    Shock Waves, 2015, 25 : 535 - 543
1234