Method for predicting rotor vortex wake and down-wash velocity field

被引:0
|
作者
Cao, Yihua
机构
关键词
D O I
暂无
中图分类号
学科分类号
摘要
Wakes
引用
收藏
页码:174 / 177
相关论文
共 34 条
  • [1] A new method for predicting rotor wake geometries and downwash velocity field
    Cao, YH
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 1999, 71 (02): : 129 - 135
  • [2] Predicting Aerodynamics and Wake Dynamics of Tilt Rotor using Unsteady Vortex Particle Method
    Son, Sang Min
    Lee, Sa-Lang
    Cho, Haeseong
    Kee, Youngjung
    Lee, Hakjin
    JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2024, 52 (10) : 775 - 787
  • [3] Spatio-temporal Distribution of Down-wash Airflow for Multi-rotor Plant Protection UAV Based on Porous Model
    Zhang H.
    Qi L.
    Wu Y.
    Liu W.
    Cheng Z.
    Musiu E.
    Nongye Jixie Xuebao/Transactions of the Chinese Society for Agricultural Machinery, 2019, 50 (02): : 112 - 122
  • [4] Modeling Rotor Wake Dynamics with Viscous Vortex Particle Method
    He, Chengjian
    Zhao, Jinggen
    AIAA JOURNAL, 2009, 47 (04) : 902 - 915
  • [5] VELOCITY-FIELD OF A CYLINDER IN THE WAKE OF A ROTOR IN FORWARD FLIGHT
    LIOU, SG
    KOMERATH, NM
    MCMAHON, HM
    JOURNAL OF AIRCRAFT, 1990, 27 (09): : 804 - 809
  • [6] Experimental Investigation of Propeller Wake Velocity Field to Determine the Major Factors Affecting Propeller Wake Wash
    Amin, Md. Asif
    Colbourne, Bruce
    Veitch, Brian
    JOURNAL OF MARINE SCIENCE AND ENGINEERING, 2018, 6 (02)
  • [7] A VORTEX EMBEDDING METHOD FOR FREE WAKE ANALYSIS OF HELICOPTER ROTOR BLADES IN HOVER
    STEINHOFF, J
    RAMACHANDRAN, K
    VERTICA, 1989, 13 (02): : 133 - 141
  • [8] Wake geometry calculations for tilt-rotor using viscous vortex method
    Shi, Y. (shiyongjie@nuaa.edu.cn), 1600, Nanjing University of Aeronautics an Astronautics (30):
  • [9] An investigation of a self-similarity for local vorticity and velocity components in tip vortex cores of a rotor wake
    Kabardin, I. K.
    Naumov, I. V.
    Okulov, V. L.
    2ND ALL-RUSSIAN SCIENTIFIC CONFERENCE THERMOPHYSICS AND PHYSICAL HYDRODYNAMICS WITH THE SCHOOL FOR YOUNG SCIENTISTS, 2017, 899
  • [10] Development of the discrete vortex cylinders method for calculating the helicopter rotor induced velocity
    Nikolaev E.I.
    Nikolaeva M.N.
    Russian Aeronautics (Iz VUZ), 2016, 59 (1) : 8 - 14