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    Modeling the Spiral Vortex Breakdown by a Solitary Wave
    螺旋型涡破裂的孤立波模型
    THE STUDY ON THE WING LEADING EDGE VORTEX BREAKDOWN
    翼前缘分离涡破裂研究
    A Calculation of Influence of Vortex Breakdown on Aerodynamic Characteristics for Slender Wings
    细长翼涡破裂对气动特性影响的计算
    The effects of vectored jet on leading edge vortex breakdown of 65° delta wing
    矢量喷流对65°三角翼前缘涡破裂的影响
    Experimental Investigation on the Leading edge Vortex Breakdown and Their Control for Flow over a 60° Delta Wing
    60°三角翼前缘涡破裂及其控制实验研究
    Experimental Studies on Leading-Edge Vortex Breakdown and Control of Flow over 76°/40° Double Delta Wing
    76°/40°双三角翼前缘涡破裂及其控制实验研究
    Effect of the apex flap on the leading edge vortex breakdownover a 70° delta wing
    尖顶襟翼对70°三角翼前缘涡破裂的影响
    Experimental investigations on the unsteady characteristics of vortex breakdown over delta wing
    三角翼涡破裂非定常特性实验研究
    Experimental analysis on oscillations of vortex breakdown location over delta wing
    三角翼前缘涡破裂点脉动的实验分析
    In the norm of angles of attack in the experiments (a<35°) ,the oscillations of the vortex-flap can largely delay the vortex-breakdown for delta wing with sweep angle of 50°;
    就实验迎角范围而言(α<35°),对50°后掠角三角翼,涡襟翼振动可显著推迟涡破裂;
    The aspect ratio H/R is 1.78 for all measurement results. Axial velocity component distribution at different Reynolds number in centerline was measured by PDA (Phase Doppler Anemometer), and the occurrence and development of vortex breakdown was quantitatively analyzed.
    实验中空腔高径比 H/R=1 .78.采用激光相位多普勒测量技术 ( Phase Doppler Anemometer,PDA)测量了圆柱空腔轴线上轴向速度分量分布随 Re变化的情况 ,定量观测和分析了涡破裂现象的发生、发展过程 ,测量到涡破裂现象出现和消失这两种临界状态 .
 

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