Effects of sweep on active separation control at high Reynolds numbers

被引：0
|
作者：
机构：
[1] Seifert, Avi
[2] Pack, LaTunia G.
来源：
Seifert, A. | 1600年 / American Inst. Aeronautics and Astronautics Inc.卷 / 40期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [31] The effects of nozzle geometry on waterjet breakup at high Reynolds numbers
    H. Vahedi Tafreshi
    B. Pourdeyhimi
    Experiments in Fluids, 2003, 35 : 364 - 371
  • [32] Investigation into the laminar separation control of airfoils at low Reynolds numbers by dimple vortex generators
    Xie, Yin
    Rao, Yu
    Cheng, Yuli
    Tian, Wei
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 129
  • [33] Control of mean and fluctuating forces on a circular cylinder at high Reynolds numbers
    Chuanping Shao Jianming Wang Institute of Mechanics
    Acta Mechanica Sinica, 2007, (02) : 133 - 143
  • [34] Control of mean and fluctuating forces on a circular cylinder at high Reynolds numbers
    Chuanping Shao Jianming Wang Institute of MechanicsChinese Academy of SciencesBeijingChina State Key Laboratory for Turbulence and Complex SystemPeking UniversityBeijing China
    Acta Mechanica Sinica, 2007, 23 (02) : 133 - 143
  • [35] Control of mean and fluctuating forces on a circular cylinder at high Reynolds numbers
    Chuanping Shao
    Jianming Wang
    Acta Mechanica Sinica, 2007, 23 : 133 - 143
  • [36] Control of mean and fluctuating forces on a circular cylinder at high Reynolds numbers
    Shao, Chuanping
    Wang, Jianming
    ACTA MECHANICA SINICA, 2007, 23 (02) : 133 - 143
  • [37] High resolution simulation of full aircraft control at flight Reynolds numbers
    Morton, Scott A.
    Forsythe, James R.
    Wurtzler, Kenneth E.
    McDaniel, David R.
    Cummings, Russell M.
    Goertz, Stefan
    Siegel, Stefan
    Squires, Kyle D.
    PROCEEDINGS OF THE HPCMP USERS GROUP CONFERENCE 2006, 2006, : 52 - 58
  • [38] High resolution simulation of full aircraft control at flight reynolds numbers
    Morton, Scott A.
    Forsythe, James R.
    McDaniel, David R.
    Bergeron, Keith
    Cummings, Russell M.
    Goertz, Stefan
    Seidel, Jurgen
    Squires, Kyle D.
    PROCEEDINGS OF THE HPCMP USERS GROUP CONFERENCE 2007, 2007, : 41 - +
  • [39] INCIPIENT SEPARATION OF A SUPERSONIC TURBULENT BOUNDARY-LAYER AT HIGH REYNOLDS-NUMBERS
    SETTLES, GS
    BOGDONOFF, SM
    VAS, IE
    AIAA JOURNAL, 1976, 14 (01) : 50 - 56
  • [40] Characterization of the Effects of Wing Sweep at Low Reynolds Number
    Nudson, Hunter
    Stanfield-Brown, Davy
    Bennett, Kylee
    Traub, Lance W.
    JOURNAL OF AIRCRAFT, 2025,
12345