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Dimension of aircraft exhaust plumes at cruise conditions: effect of wake vortices

机译:巡航条件下飞机尾气羽流的尺寸:尾流涡流的影响

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摘要

The dispersion of aircraft emissions during the vortex phase is studied using a 3-D LES model with Lagrangian particle tracking. The simulations start with a fully rolled-up vortex pair of a type B747/A340 airplane and the tracer centred around the vortex cores. The tracer dilution and plume extent is studied for a variety of ambient and aircraft parameters until aircraft-induced effects have ceased. For typical upper tropospheric conditions, the impact of stratification is more dominant compared to turbulence intensity or vertical wind shear. Moreover, the sensitivity to the initial tracer distribution was found to be weak. Along the transverse direction, the tracer concentrations can be well approximated by a Gaussian distribution, along the vertical a superposition of three Gaussian distributions is adequate.
机译:使用带有拉格朗日粒子跟踪的3-D LES模型研究了旋涡阶段飞机排放的弥散。模拟从B747 / A340型飞机的完全卷起的涡流对开始,示踪剂围绕涡流核居中。研究示踪剂的稀释度和羽流程度,以了解各种环境和飞机参数,直到飞机引起的影响消失为止。对于典型的对流层高空条件,与湍流强度或垂直风切变相比,分层的影响更为明显。此外,发现对初始示踪剂分布的敏感性较弱。沿着横向方向,示踪剂浓度可以通过高斯分布很好地近似,沿着垂直方向,三个高斯分布的叠加是足够的。

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