Low Reynolds unsteady flow simulation around NACA0012 airfoil with active flow control

被引:0
|
作者
Faculty of Mechanical and Mechatronics Engineering, Shahrood University of Technology, P.Box: 3619995161, Shahrood [1 ]
Semnan, Iran
机构
来源
Meccanica | / 14卷 / 3457-3476期
关键词
Compilation and indexing terms; Copyright 2024 Elsevier Inc;
D O I
暂无
中图分类号
学科分类号
摘要
Lift - C++ (programming language) - Reynolds number - Angle of attack - Computer software - Drag reduction - Numerical methods - Aerodynamic stalling - Incompressible flow - Flow control
引用
收藏
相关论文
共 50 条
  • [41] First stages of the transition to turbulence and control in the incompressible detached flow around a NACA0012 wing
    Hoarau, Y.
    Braza, M.
    Ventikos, Y.
    Faghani, D.
    [J]. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2006, 27 (05) : 878 - 886
  • [42] Mode and regime identification for a static NACA0012 airfoil at transitional Reynolds numbers
    Poels, Allison
    Collin, Xavier
    Benaissa, Azemi
    Poirel, Dominique
    [J]. MECHANICS & INDUSTRY, 2020, 21 (06)
  • [43] Investigation on effect of square dimples on NACA0012 airfoil with various Reynolds numbers
    Joseph, D. Raja
    Devi, P. Booma
    Gopalsamy, M.
    [J]. INTERNATIONAL JOURNAL OF AMBIENT ENERGY, 2021, 42 (04) : 397 - 402
  • [44] LBM-LES Modelling of Low Reynolds Number Turbulent Flow Over NACA0012 Aerofoil
    Nadim, Nima
    Chandratilleke, Tilak T.
    Krause, Mathias J.
    [J]. FLUID-STRUCTURE-SOUND INTERACTIONS AND CONTROL, 2016, : 205 - 210
  • [45] Influence of Turbulence Intensity on Flow Field Around NACA0012 Wing at Reynolds Number of 20,000
    Kase, Masataka
    Mizoguchi, Makoto
    Itoh, Hajime
    [J]. PROCEEDINGS OF THE 2021 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY (APISAT 2021), VOL 1, 2023, 912 : 505 - 511
  • [46] Influence of heat transfer on the aerodynamic performance of a plunging and pitching NACA0012 airfoil at low Reynolds numbers
    Hinz, Denis F.
    Alighanbari, Hekmat
    Breitsamter, Christian
    [J]. JOURNAL OF FLUIDS AND STRUCTURES, 2013, 37 : 88 - 99
  • [47] Hysteresis in flow past a NACA 0012 airfoil
    Mittal, S
    Saxena, P
    [J]. COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2002, 191 (19-20) : 2179 - 2189
  • [48] Localization of Flow Separation and Transition Over a Pitching NACA0012 Airfoil at Transitional Reynolds Numbers Using Hot-Films
    Poels, Allison
    Rudmin, Daniel
    Benaissa, Azemi
    Poirel, Dominique
    [J]. JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2015, 137 (12):
  • [49] Self-sustained aeroelastic oscillations of a NACA0012 airfoil at low-to-moderate Reynolds numbers
    Poirel, D.
    Harris, Y.
    Benaissa, A.
    [J]. JOURNAL OF FLUIDS AND STRUCTURES, 2008, 24 (05) : 700 - 719
  • [50] Numerical study of blowing and suction control mechanism on NACA0012 airfoil
    Huang, L
    Huang, PG
    LeBeau, RRP
    Hauser, T
    [J]. JOURNAL OF AIRCRAFT, 2004, 41 (05): : 1005 - 1013