Reynolds number effects on vortex breakdown of a blunt-edged delta

被引:2
|
作者
Traub, LW
Galls, SF
Rediniotis, OK
机构
[1] Texas A and M University, College Station
来源
JOURNAL OF AIRCRAFT | 1996年 / 33卷 / 04期
关键词
D O I
10.2514/3.47025
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:835 / 837
页数:3
相关论文
共 50 条
  • [1] Influences of angle of attack, Reynolds number and leading edge bluntness on inner vortex characterization of blunt-edged VFE-2 delta wing
    Tajuddin, Nurulhuda
    Said, Mazuriah
    Musa, Nur Amalina
    Mat, Shabudin
    Wong, Kok Hoe
    Kasim, Khushairi Amri
    Ramli, Yahaya
    Ali, Airi
    Mansor, Shuhaimi
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2025,
  • [2] Effects of Leading Edge Enlargement on the Primary Vortex of Blunt-Edged Delta Wing VFE-2 Profile
    Said, Mazuriah
    Mat, Shabudin
    Mansor, Shuhaimi
    Ali, Airi
    ACTA POLYTECHNICA HUNGARICA, 2018, 15 (08) : 7 - 28
  • [3] Blunt-edged, notched scalpel for cesarean incision
    Ishii, S
    Endo, M
    OBSTETRICS AND GYNECOLOGY, 1999, 94 (03): : 469 - 470
  • [4] Influence of Active Flow Control on Blunt-Edged VFE-2 Delta Wing model
    Madan, I
    Tajuddin, N.
    Said, M.
    Mat, S.
    Othman, N.
    Wahid, M. A.
    Radzi, N. H. Mohamed
    Miau, J. J.
    Chen, Y. R.
    Chen, L. Y.
    INTERNATIONAL JOURNAL OF AUTOMOTIVE AND MECHANICAL ENGINEERING, 2021, 18 (01) : 8411 - 8422
  • [5] Experiment investigation on vortex breakdown at different Reynolds number
    Liu, Yingzheng
    Chen, Hanping
    Luo, Cishen
    Jin, Hao
    Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2000, 34 (04): : 513 - 516
  • [6] Onset of chaos in helical vortex breakdown at low Reynolds number
    Pasche, S.
    Avellan, F.
    Gallaire, F.
    PHYSICAL REVIEW FLUIDS, 2018, 3 (06):
  • [7] Mach-Number Effects on Vortex Breakdown in Subsonic Flows over Delta Wings
    Nonomura, Taku
    Fukumoto, Hiroaki
    Ishikawa, Yoshihiro
    Fujii, Kozo
    AIAA JOURNAL, 2013, 51 (09) : 2281 - 2286
  • [8] The blunt-edged sword: genetic explanations of misbehavior neither mitigate nor aggravate punishment
    Scurich, Nicholas
    Appelbaum, Paul
    JOURNAL OF LAW AND THE BIOSCIENCES, 2016, 3 (01): : 140 - 157
  • [9] Shock Effects on Delta Wing Vortex Breakdown
    Schiavetta, L. A.
    Boelens, O. J.
    Crippa, S.
    Cummings, R. M.
    Fritz, W.
    Badcock, K. J.
    JOURNAL OF AIRCRAFT, 2009, 46 (03): : 903 - 914
  • [10] Shock effects on delta wing vortex breakdown
    Schiavetta, L.A.
    Boelens, O.J.
    Crippa, S.
    Cummings, R.M.
    Fritz, W.
    Badcock, K.J.
    Journal of Aircraft, 2009, 46 (03): : 903 - 914