FLOW SEPARATION AND VORTEX BURSTING LOCATIONS ON WINGS PITCHING AT CONSTANT RATES

被引:0
|
作者
HUDSON, LJ
KING, PI
DAVID, M
机构
关键词
D O I
暂无
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:1 / 7
页数:7
相关论文
共 50 条
  • [31] SUBSONIC VORTEX-FLOW DESIGN STUDY FOR SLENDER WINGS
    LAMAR, JE
    ASTRONAUTICS & AERONAUTICS, 1978, 16 (11): : B41 - B41
  • [32] SUBSONIC VORTEX-FLOW DESIGN STUDY FOR SLENDER WINGS
    LAMAR, JE
    JOURNAL OF AIRCRAFT, 1978, 15 (09): : 611 - 617
  • [33] Investigation of Vortex Structures in the Supersonic Flow around a Tandem of Wings
    Borisov V.E.
    Konstantinovskaya T.V.
    Lutsky A.E.
    Mathematical Models and Computer Simulations, 2023, 15 (1) : 59 - 72
  • [34] EFFICIENCY OF ENERGY SEPARATION IN A VORTEX FLOW
    Tyutyuma, V. D.
    JOURNAL OF ENGINEERING PHYSICS AND THERMOPHYSICS, 2016, 89 (02) : 422 - 427
  • [35] Parametrical study on separation-induced transition and vortex dynamics of a reversed pitching airfoil
    Shi, Lei
    Wang, Yefang
    Zhang, Desheng
    Bayeul-Laine, Annie-Claude
    Coutier-Delgosha, Olivier
    OCEAN ENGINEERING, 2022, 264
  • [36] VORTEX FLOW BEHIND AN UNSTEADY AIRFOIL IN PITCHING AND HEAVING MOTIONS AND DYNAMIC THRUST
    Fuchiwaki, Masaki
    Tanaka, Kazuhiro
    PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER CONFERENCE, VOL 2, 2006, : 737 - 742
  • [37] COMPUTATION OF VORTEX-DOMINATED FLOW FOR A DELTA WING UNDERGOING PITCHING OSCILLATION
    KANDIL, OA
    CHUANG, HA
    AIAA JOURNAL, 1990, 28 (09) : 1589 - 1595
  • [38] Numerical investigations of the vortex interactions for a flow over a pitching foil at different stages
    Tseng, Chien-Chou
    Cheng, Yu-En
    JOURNAL OF FLUIDS AND STRUCTURES, 2015, 58 : 291 - 318
  • [39] Development of a wind tunnel experiment for vortex dominated flow at a pitching Lambda wing
    Wiggen S.
    Voß G.
    CEAS Aeronautical Journal, 2014, 5 (4) : 477 - 486
  • [40] EXPERIMENTAL INVESTIGATIONS OF THE VORTEX FLOW ON DELTA WINGS AT HIGH-INCIDENCE
    STAHL, WH
    MAHMOOD, M
    ASGHAR, A
    AIAA JOURNAL, 1992, 30 (04) : 1027 - 1032