VISUALIZATION OF THE WING-TIP VORTEX IN TEMPORAL AND SPATIAL PRESSURE-GRADIENTS

被引:3
|
作者
LIANG, X
RAMAPRIAN, BR
机构
[1] TSING HUA UNIV,DEPT THERMAL ENGN,BEIJING,PEOPLES R CHINA
[2] WASHINGTON STATE UNIV,DEPT MECH & MAT ENGN,PULLMAN,WA 99164
关键词
D O I
10.1115/1.2909527
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The evolution of the longitudinal vortex in the near field of a rectangular wing has been visualized using smoke and laser light sheet. The smoke photographs have been used to obtain qualitative and some quantitative information on the effect of small temporal and spatial pressure gradients on the evolution of the vortex in this region. The experiments indicate that even small temporal retardation of the flow can produce a significant increase in the vortex size. This effect becomes larger with increase in retardation, angle of incidence and distance downstream from the trailing edge. Also, vortex "breakdown" was found to occur in many temporal-deceleration experiments. The vortex evolution was, however, found to be relatively insensitive to the presence of small spatial adverse pressure gradients along the flow direction. The study is preliminary in nature and needs to be supported by more extensive quantitative measurements.
引用
收藏
页码:511 / 515
页数:5
相关论文
共 50 条
  • [21] Numerical study of a wing-tip vortex using the Euler equations
    Spall, RE
    JOURNAL OF AIRCRAFT, 2001, 38 (01): : 22 - 27
  • [22] Turbulence structure resulting from a vortex/wing-tip encounter
    Wittmer, KS
    Devenport, WJ
    Wenger, CW
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1999, 44 (02) : 141 - 149
  • [23] Effect of dielectric barrier discharge on wing-tip vortex formation
    S. A. Agibalova
    V. V. Golub
    I. A. Moralev
    A. S. Saveliev
    Technical Physics Letters, 2011, 37 : 1070 - 1073
  • [24] Wing-Tip Vortex Jet Interaction in the Extended Near Field
    Zurheide, Frank T.
    Meinke, Matthias
    Schroeder, Wolfgang
    HIGH PERFORMANCE COMPUTING IN SCIENCE AND ENGINEERING '08, 2009, : 269 - 283
  • [25] Visualization and PIV study of wing-tip vortices for three different tip configurations
    Sohn, Myong Hwan
    Chang, Jo Won
    AEROSPACE SCIENCE AND TECHNOLOGY, 2012, 16 (01) : 40 - 46
  • [26] THE INFLUENCE OF THE AXIAL PRESSURE-GRADIENTS ON THE BREAKDOWN OF A VORTEX
    KRAUSE, E
    ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1984, 64 (04): : T207 - T208
  • [27] Near field study of vortex attenuation using wing-tip blowing
    Simpson, RG
    Ahmed, NA
    Archer, RD
    AERONAUTICAL JOURNAL, 2002, 106 (1057): : 117 - 120
  • [28] Measurements of the velocity field of a wing-tip vortex, wandering in grid turbulence
    Bailey, S. C. C.
    Tavoularis, S.
    JOURNAL OF FLUID MECHANICS, 2008, 601 (281-315) : 281 - 315
  • [29] Correction of wandering smoothing effects on static measurements of a wing-tip vortex
    Giacomo Valerio Iungo
    Peter Skinner
    Guido Buresti
    Experiments in Fluids, 2009, 46 : 435 - 452
  • [30] Near-field wing-tip vortices and exponential vortex solution
    Zhana, HJ
    Zhou, Y
    Whitelaw, JH
    JOURNAL OF AIRCRAFT, 2006, 43 (02): : 445 - 449