Separation Topology of Microramp Vortex Generator Controlled Flow at Mach Number 2.5

被引：7
|
作者：
Li, Qin [1 ,2 ]
Yan, Yonghua [2 ]
Liu, Chaoqun [2 ]
Lu, Frank [3 ]
机构：
[1] State Key Lab Aerodynam, Mianyang 621000, Peoples R China
[2] Univ Texas Arlington, Dept Math, Arlington, TX 76019 USA
[3] Univ Texas Arlington, Dept Mech & Aerosp Engn, Arlington, TX 76019 USA
来源：
JOURNAL OF AIRCRAFT | 2015年 / 52卷 / 06期
基金：
美国国家科学基金会;
关键词：
D O I：
10.2514/1.C033280
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：2095 / 2099
页数：5
相关论文
共 50 条
  • [21] Numerical Study of Flow Separation Control in Waterjet Intake Duct by Vortex Generator
    Huang C.-L.
    Chen L.
    Wang Z.-L.
    Dai R.
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (07):
  • [22] Study on influence of vortex generator on flow separation characteristics of tidal turbine blades
    Liu Y.
    Zhe H.
    Tan J.
    Si X.
    Yuan P.
    Wang S.
    Taiyangneng Xuebao/Acta Energiae Solaris Sinica, 2022, 43 (11): : 358 - 363
  • [23] Numerical Investigation of Steady and Harmonic Vortex Generator Jets Flow Separation Control
    Alimi, Aria
    Wuensch, Olaf
    FLUIDS, 2018, 3 (04):
  • [24] Steady and pulsed vortex generator jets control of flow separation in rectangle diffuser
    Xie, Yonghui
    Fan, Tao
    Zhang, Di
    Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2010, 44 (11): : 1 - 5
  • [25] Statistical Vortex-Generator-Jet Model for Turbulent Flow Separation Control
    von Stillfried, Florian
    Wallin, Stefan
    Johansson, Arne V.
    AIAA JOURNAL, 2013, 51 (05) : 1119 - 1129
  • [26] Analysis of the Effect of Vortex Generator Spacing on Boundary Layer Flow Separation Control
    Li, Xin-kai
    Liu, Wei
    Zhang, Ting-jun
    Wang, Pei-ming
    Wang, Xiao-dong
    APPLIED SCIENCES-BASEL, 2019, 9 (24):
  • [27] Numerical Study on Suppression of Intake Flow Separation Using Vortex Generator Jet
    Zhou Y.-Y.
    Chen L.
    Luo J.-W.
    Tuijin Jishu/Journal of Propulsion Technology, 2023, 44 (08):
  • [28] Vortex sound in the presence of a low Mach number flow across a drum-like silencer
    Tang, S. K.
    JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 2011, 129 (05): : 2830 - 2840
  • [29] Vortex sound due to a flexible boundary backed by a cavity in a low Mach number mean flow
    Tang, S. K.
    Leung, R. C. K.
    So, R. M. C.
    JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 2007, 121 (03): : 1345 - 1352
  • [30] Suppressing a Laminar Flow Separation Zone by Spark Discharge at Mach Number M=1.43
    Polivanov, P. A.
    Sidorenko, A. A.
    TECHNICAL PHYSICS LETTERS, 2018, 44 (09) : 833 - 836
12345