Effect of canards on delta wing vortex breakdown during dynamic pitching

被引：0
|
作者：
Wichita State Univ, Wichita, United States [1 ]
机构：
来源：
J Aircr | / 2卷 / 168-173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
  • [21] Effect of fuselage geometry on delta-wing vortex breakdown
    AIAA, United States
    J Aircr, 6 (898-904):
  • [22] EFFECT OF FUSELAGE ON DELTA-WING VORTEX BREAKDOWN - COMMENT
    ERICSSON, LE
    JOURNAL OF AIRCRAFT, 1994, 31 (04): : 1006 - 1007
  • [23] Effect of fuselage geometry on delta-wing vortex breakdown
    Ericsson, LE
    JOURNAL OF AIRCRAFT, 1998, 35 (06): : 898 - 904
  • [24] EFFECTS OF BLOWING ON DELTA-WING VORTICES DURING DYNAMIC PITCHING
    MILLER, LS
    GILE, BE
    JOURNAL OF AIRCRAFT, 1993, 30 (03): : 334 - 339
  • [25] 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
  • [26] Computation of vortex breakdown on a rolling delta wing
    Gordnier, R.E., 1600, American Institute of Aeronautics and Astronautics Inc. (32):
  • [27] 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
  • [28] Numerical investigation of vortex breakdown on a delta wing
    Agrawal, Shreekant
    Barnett, Raymond Matt
    Robinson, Brian Anthony
    AIAA journal, 1992, 30 (03): : 584 - 591
  • [29] 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
  • [30] Impact of initial conditions on vortex breakdown on pitching delta wings
    Ericsson, LE
    JOURNAL OF AIRCRAFT, 1997, 34 (03): : 452 - 454
12345