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
  • [31] Vortex shedding from tapered plates
    I. Castro
    P. Rogers
    Experiments in Fluids, 2002, 33 : 66 - 74
  • [32] EXPERIMENTAL AND THEORETICAL INVESTIGATIONS ON THE VORTEX FORMATION OVER DOUBLE-DELTA WINGS
    BRENNENSTUHL, U
    HUMMEL, D
    ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1987, 11 (01): : 37 - 49
  • [33] Vortex shedding from rectangular plates
    Yakhot, Alexander
    Nikitin, Nikolai
    Liu, Heping
    AIAA Journal, 2004, 42 (07): : 1489 - 1491
  • [34] Vortex shedding from tapered plates
    Castro, IP
    Rogers, P
    EXPERIMENTS IN FLUIDS, 2002, 33 (01) : 66 - 74
  • [35] Symmetry breaking and instabilities of conical vortex pairs over slender delta wings
    Ma, Bao-Feng
    Wang, Zhijin
    Gursul, Ismet
    JOURNAL OF FLUID MECHANICS, 2017, 832 : 41 - 72
  • [36] Experimental investigations on vortex breakdown over delta wings with Doppler global velocimetry
    Förstermann, M
    Bütefisch, KA
    ICIASF'99: INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES, RECORD, 1999, : 101 - 1010
  • [37] Numerical simulation of vortical flows over delta wings and analysis of vortex motion
    Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 1997, 15 (01): : 121 - 129
  • [38] AERODYNAMIC FORCE MEASUREMENT ON CARET AND DELTA WINGS AT HIGH INCIDENCE
    COLEMAN, GT
    JOURNAL OF SPACECRAFT AND ROCKETS, 1973, 10 (11) : 750 - 751
  • [39] Criteria for Vortex Breakdown Above High-Sweep Delta Wings
    Jones, Michael
    Hashimoto, Atsushi
    Nakamura, Yoshiaki
    AIAA JOURNAL, 2009, 47 (10) : 2306 - 2320
  • [40] Computation of field structure and aerodynamic characteristics of delta wings at high angles of attack
    Yang, LZ
    Gao, ZH
    APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2005, 26 (06) : 797 - 806
12345