VORTEX SHEDDING OVER DELTA WINGS AND PLATES AT HIGH ANGLES OF INCIDENCE

被引：0
|
作者：
STAPOUNTZIS, H
ILIADIS, G
AGELAKIS, J
MANSOUR, G
机构：
来源：
ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG | 1992年 / 16卷 / 05期
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Hot wire measurements in the wake of bodies with sharp edges are presented. The edges were inclined (delta wing) or parallel (square, rectangular plates) with bevel against or with the flow. The nature of vortex shedding at various angles of incidence and Reynolds number was investigated by analysis of the cross power spectral density of the two hot wire signals. The delta wing is characterized by both alternate and simultaneous vortex shedding.
引用
收藏
页码：331 / 341
页数：11
相关论文
共 50 条
  • [1] VORTEX SHEDDING OVER DELTA-WINGS
    REDINIOTIS, OK
    STAPOUNTZIS, H
    TELIONIS, DP
    AIAA JOURNAL, 1990, 28 (05) : 944 - 946
  • [2] PERIODIC VORTEX SHEDDING OVER DELTA-WINGS
    REDINIOTIS, OK
    STAPOUNTZIS, H
    TELIONIS, DP
    AIAA JOURNAL, 1993, 31 (09) : 1555 - 1562
  • [3] VORTEX INTERACTION OVER DOUBLE DELTA-WINGS AT HIGH ANGLES OF ATTACK
    OLSEN, PE
    NELSON, RC
    AIAA 7TH APPLIED AERODYNAMICS CONFERENCE: A COLLECTION OF TECHNICAL PAPERS, 1989, : 238 - 248
  • [4] Asymmetrical vortex breakdown of delta wings at high incidence
    Xiao, Zhi-Xiang
    Chen, Hai-Xin
    Fu, Song
    Li, Feng-Wei
    Jisuan Wuli/Chinese Journal of Computational Physics, 2005, 22 (03): : 221 - 226
  • [5] EXPERIMENTAL INVESTIGATIONS OF THE VORTEX FLOW ON DELTA WINGS AT HIGH-INCIDENCE
    STAHL, WH
    MAHMOOD, M
    ASGHAR, A
    AIAA JOURNAL, 1992, 30 (04) : 1027 - 1032
  • [6] Origin of vortex wandering over delta wings
    Gursul, I
    Xie, WS
    JOURNAL OF AIRCRAFT, 2000, 37 (02): : 348 - 350
  • [7] THE CONTROL OF ASYMMETRIC VORTICAL FLOWS OVER DELTA WINGS AT HIGH ANGLES OF ATTACK
    WOOD, NJ
    ROBERTS, L
    CELIK, Z
    AIAA ATMOSPHERIC FLIGHT MECHANICS CONFERENCE: A COLLECTION OF TECHNICAL PAPERS, 1989, : 484 - 491
  • [8] VORTEX FLOW OVER DELTA AND DOUBLE-DELTA WINGS
    HOEIJMAKERS, HWM
    VAATSTRA, W
    VERHAAGEN, NG
    JOURNAL OF AIRCRAFT, 1983, 20 (09): : 825 - 832
  • [9] COMPARISON OF LIFT OF FLAT DELTA WINGS AND WAVERIDERS AT HIGH ANGLES OF INCIDENCE AND HIGH MACH NUMBER
    SQUIRE, LC
    INGENIEUR ARCHIV, 1971, 40 (05): : 339 - &
  • [10] CONTROL OF ASYMMETRIC VORTICAL FLOWS OVER DELTA-WINGS AT HIGH ANGLES OF ATTACK
    WOOD, NJ
    ROBERTS, L
    CELIK, Z
    JOURNAL OF AIRCRAFT, 1990, 27 (05): : 429 - 435
12345