对一次东移高原低涡减弱、高原切变线生成并在有利的环流背景下东南移,进而引发川渝强降水的高原切变线生成机制以及演变过程进行了初步分析。首先引入描写热带气旋的Okubo-Weiss(OW)参数(VOW)来定量表达低涡、切变气流中旋转和变形的...对一次东移高原低涡减弱、高原切变线生成并在有利的环流背景下东南移,进而引发川渝强降水的高原切变线生成机制以及演变过程进行了初步分析。首先引入描写热带气旋的Okubo-Weiss(OW)参数(VOW)来定量表达低涡、切变气流中旋转和变形的相对大小,确定高原切变线的潜在生成区域和发展状况。得出在高原切变线生成阶段,500 h Pa等压面上VOW值由正转负,VOW负值带可以很好地指示高原切变线的潜在生成区域。VOW负值强度与高原切变线强度有很好的相关性。高原切变线上以VOW负值中心为主,但也会存在正值中心,说明在切变线上也会有气旋性涡度。此个例高原切变线以伸缩变形为主,高原切变线沿变形场的拉伸轴分布。然后通过涡度方程和总变形方程进一步分析了高原低涡减弱、高原切变线生成的动力机制。高原低涡的减弱、消失主要受散度项的影响,时间演变分析表明系统由强气旋性涡度的高原低涡演变为强辐合性的高原切变线。总变形方程中的扭转项对高原切变线的生成贡献最大,其次为水平气压梯度项,散度项最小;当高原切变线上以拉伸变形为主时,不利于其上高原低涡的发展,切变线可能是影响低涡发展的背景流场。展开更多
Wake separation is crucial to aircraft landing safety and is an important factor in airport operational efficiency.The near-ground evolution characteristics of wake vortices form the foundation of the wake separation ...Wake separation is crucial to aircraft landing safety and is an important factor in airport operational efficiency.The near-ground evolution characteristics of wake vortices form the foundation of the wake separation system design.In this study,we analysed the near-ground evolution of vortices in the wake of a domestic aircraft ARJ21 initialised by the lift-drag model using large eddy simulations based on an adaptive mesh.Evolution of wake vortices formed by the main wing,flap and horizontal tail was discussed in detail.The horizontal tail vortices are the weakest and dissipate rapidly,whereas the flap vortices are the strongest and induce the tip vortex to merge with them.The horizontal tail and flap of an ARJ21 do not significantly influence the circulation evolution,height change and movement trajectory of the wake vortices.The far-field evolution of wake vortices can therefore be analysed using the conventional wake vortex model.展开更多
The fine space-time structure of a vortex generator （VG） in supersonic flow is studied with the nanoparticle-based planar laser scattering （NPLS） method in a quiet supersonic wind tunnel. The fine coherent structu...The fine space-time structure of a vortex generator （VG） in supersonic flow is studied with the nanoparticle-based planar laser scattering （NPLS） method in a quiet supersonic wind tunnel. The fine coherent structure at the symmetrical plane of the flow field around the VG is imaged with NPLS. The spatial structure and temporal evolution characteristics of the vortical structure are analyzed, which demonstrate periodic evolution and similar geometry, and the characteristics of rapid movement and slow change. Because the NPLS system yields the flow images at high temporal and spatial resolutions, from these images the position of a large scale structure can be extracted precisely. The position and velocity of the large scale structures can be evaluated with edge detection and correlation algorithms. The shocklet structures induced by vortices are imaged, from which the generation and development of shocklets are discussed in this paper.展开更多
文摘对一次东移高原低涡减弱、高原切变线生成并在有利的环流背景下东南移,进而引发川渝强降水的高原切变线生成机制以及演变过程进行了初步分析。首先引入描写热带气旋的Okubo-Weiss(OW)参数(VOW)来定量表达低涡、切变气流中旋转和变形的相对大小,确定高原切变线的潜在生成区域和发展状况。得出在高原切变线生成阶段,500 h Pa等压面上VOW值由正转负,VOW负值带可以很好地指示高原切变线的潜在生成区域。VOW负值强度与高原切变线强度有很好的相关性。高原切变线上以VOW负值中心为主,但也会存在正值中心,说明在切变线上也会有气旋性涡度。此个例高原切变线以伸缩变形为主,高原切变线沿变形场的拉伸轴分布。然后通过涡度方程和总变形方程进一步分析了高原低涡减弱、高原切变线生成的动力机制。高原低涡的减弱、消失主要受散度项的影响,时间演变分析表明系统由强气旋性涡度的高原低涡演变为强辐合性的高原切变线。总变形方程中的扭转项对高原切变线的生成贡献最大,其次为水平气压梯度项,散度项最小;当高原切变线上以拉伸变形为主时,不利于其上高原低涡的发展,切变线可能是影响低涡发展的背景流场。
基金financial support from the National Natural Science Foundation of China(Grant 91752205)Civil Aviation Joint Fund of NSFC(Grant U1733203)Civil Aviation Safety Capacity Building Project(Grant TM 2019-16-1/3)。
文摘Wake separation is crucial to aircraft landing safety and is an important factor in airport operational efficiency.The near-ground evolution characteristics of wake vortices form the foundation of the wake separation system design.In this study,we analysed the near-ground evolution of vortices in the wake of a domestic aircraft ARJ21 initialised by the lift-drag model using large eddy simulations based on an adaptive mesh.Evolution of wake vortices formed by the main wing,flap and horizontal tail was discussed in detail.The horizontal tail vortices are the weakest and dissipate rapidly,whereas the flap vortices are the strongest and induce the tip vortex to merge with them.The horizontal tail and flap of an ARJ21 do not significantly influence the circulation evolution,height change and movement trajectory of the wake vortices.The far-field evolution of wake vortices can therefore be analysed using the conventional wake vortex model.
基金National Natural Science Foundation of China(11072264)
文摘The fine space-time structure of a vortex generator （VG） in supersonic flow is studied with the nanoparticle-based planar laser scattering （NPLS） method in a quiet supersonic wind tunnel. The fine coherent structure at the symmetrical plane of the flow field around the VG is imaged with NPLS. The spatial structure and temporal evolution characteristics of the vortical structure are analyzed, which demonstrate periodic evolution and similar geometry, and the characteristics of rapid movement and slow change. Because the NPLS system yields the flow images at high temporal and spatial resolutions, from these images the position of a large scale structure can be extracted precisely. The position and velocity of the large scale structures can be evaluated with edge detection and correlation algorithms. The shocklet structures induced by vortices are imaged, from which the generation and development of shocklets are discussed in this paper.
