Unsteady vortex breakdown behaviour over a pitching-rolling 70° delta wing

被引:0
|
作者
Kowal, H.J. [1 ]
Vakili, A.D. [2 ]
机构
[1] 14 Air Maintenance Squadron, 14 Wing Greenwood, Nova Scotta, Tullahoma, TN, United States
[2] Univ. of Tennessee Space Institute, Tullahoma, TN, United States
来源
| 2000年 / CASI, Ottawa, Canada卷 / 46期
关键词
D O I
暂无
中图分类号
学科分类号
摘要
20
引用
收藏
相关论文
共 50 条
  • [41] The effect of blowing on control of vortex breakdown over a delta wing.
    Rodriguez, O
    Pruvost, J
    COMPTES RENDUS MECANIQUE, 2005, 333 (10): : 773 - 777
  • [42] Forebody slot blowing on vortex breakdown and load over a delta wing
    Cui, Y. D.
    Lim, T. T.
    Tsai, H. M.
    AIAA JOURNAL, 2008, 46 (03) : 744 - 751
  • [43] AN EVALUATION OF TURBULENCE MODEL FOR VORTEX BREAKDOWN DETECTION OVER DELTA WING
    Wibowo, Setyawan Bekti
    Sutrisno
    Rohmat, Tri Agung
    ARCHIVE OF MECHANICAL ENGINEERING, 2018, 65 (03) : 399 - 415
  • [44] Vortex breakdown over a delta wing with oscillating leading edge flaps
    Q. Deng
    I. Gursul
    Experiments in Fluids, 1997, 23 : 347 - 352
  • [45] Analysis of Shock and Vortex Breakdown Behavior in Unsteady Transonic Flow on A Slender Delta Wing
    Li Xile
    Yang Yong
    Jiao Jin
    PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2, 2010, : 444 - 447
  • [46] EXPERIMENTS AND ANALYSIS OF HYSTERESIS OF VORTEX BREAKDOWN OVER PITCHING-UP DELTA WINGS
    Yang Xiaofeng
    L■ Zhiyong(Institute of Fluid Mechanics
    Chinese Journal of Aeronautics, 1997, (01) : 9 - 13
  • [47] Effects of unsteady freestream on aerodynamic characteristics of pitching delta wing
    Shi, Zhi-Wei
    Ming, Xiao
    Journal of Aircraft, 1600, 45 (06): : 2182 - 2185
  • [48] Effects of Unsteady Freestream on Aerodynamic Characteristics of Pitching Delta Wing
    Shi, Zhi-Wei
    Ming, Xiao
    JOURNAL OF AIRCRAFT, 2008, 45 (06): : 2182 - 2185
  • [49] 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
  • [50] Effect of a fuselage on delta wing vortex breakdown
    Straka, William A.
    Hemsch, Michael J.
    1600, AIAA, Washington, DC, United States (31):