Numerical study of aircraft wake vortex evolution near ground in stable atmospheric boundary layer

作者：Lin, Mengda; Huang, Weixi; Zhang, Zhaoshun; Xu, Chunxiao; Cui, Guixiang^*

来源：Chinese Journal of Aeronautics, 2017, 30(6): 1866-1876.

DOI：10.1016/j.cja.2017.08.012

• Aerodynamics
• Aircraft
• Aircraft wake vortex
• Large eddy simulation
• Stable atmosphere boundary layer

The evolutions of aircraft wake vortices near ground in stable atmospheric boundary layer are studied by Large Eddy Simulation (LES). The sensitivity of vortex evolution to the Monin-Obukhov (M-O) scale is studied for the first time. The results indicate that increasing stability leads to longer lifetimes of upwind vortices, while downwind vortices will decay faster due to a stronger crosswind shear under stable conditions. Based on these results, an empirical model of the vortex lifetime as a function of 10-m-high crosswind and the M-O scale is summarized. This model can provide an estimate of the upper boundary of the vortex lifetime according to the realtime crosswind and atmospheric stability. In addition, the lateral translation of vortices is also inspected. The results show that vortices can travel a furthest distance of 722 m in the currently studied parameter range. This result is meaningful to safety analysis of airports that have parallel runways.

• 出版日期2017-12
• 单位清华大学