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Editorial note on Interplay of unsteady aerodynamics and flight dynamics of transport aircraft in icing conditions

机译:关于运输飞机在结冰条件下的不稳定空气动力学和飞行动力学的相互作用的编辑记录

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A field study on the aerodynamics of freight trains to determine the aerodynamic efficiency of shipping containers loaded on intermodal freight trains, a novel full-scale field test was performed. In the sense of surface pressure, weather stations, and GPS data sets, the aerodynamic efficiency of an instrumented 48 ft container located 185 m downstream of the locomotive is evaluated. There have been previous research on train aerodynamics. Previous research on train aerodynamics has largely been limited to low-resolution, reduced-order, and scaled field, numerical, and wind-tunnel studies. The goal of this study was to see how well this new field-based approach could determine the aerodynamic efficiency of full-scale train containers under a variety of conditions. The calculated surface pressure distributions on the front and base of the container are close to those of previous work in low wind conditions where the yaw angle is expected to be low, but the magnitude of the drag coefficient was much lower, by up to 65 percent. This indicates that previous research hasn't gone into enough detail about the drag profile of containers located far downstream. A new propeller called Boxprop, with blade tips joined in pairs, is planned and optimised for a conceptual electric aircraft using an effective framework for optimization. The Boxprop with optimum efficiency is down-selected from the Pareto front of thrust coefficient and propeller efficiency in accordance with the thrust requirement of the electric aircraft at cruise. Subsequently, the aeroacoustic analysis performed by the Reynolds-Averaged Navier Stokes (RANS) hybrid integral system and the Williams and Hawkings (FW-H) convected Ffowcs (FWH) equation shows that the tonal noise from the Boxprop with three joined cruise blades is similar to a traditional three-bladed propeller, but greater than a conventional six-bladed propeller.
机译:对货运训练的空气动力学的田间研究,以确定在多式联运训练上装载在多式联运货物上的运输容器的空气动力学效率,进行了一种新的全规模场测试。在表面压力,气象站和GPS数据集的意义上,评估位于机车下游185米的仪器48 FT容器的空气动力学效率。以前有关于火车空气动力学的研究。以前关于火车空气动力学的研究基本上限于低分辨率,减少阶和缩放的现场,数值和风洞研究。本研究的目标是看出这种基于领域的方法如何在各种条件下确定全规模列车容器的空气动力学效率。容器前部和底部的计算的表面压力分布接近先前的工作中的工作中的那些,其中偏航角预计越低,但拖曳系数的大小远低得多,高达65% 。这表明前面的研究尚未对位于下游的容器的拖动轮廓陷入足够的细节。使用有效的优化框架,计划和优化一个名为Boxprop的新螺旋桨,并针对成对加入的刀片提示,并针对概念性的电动机进行了优化。通过电气飞机在巡航中的推力要求,从普通效率和螺旋桨效率的Pareto前面选择了最佳效率的Boxprop。随后,由Reynolds-Iveriged Navier Stokes(RANS)混合积分系统和威廉姆斯和霍普林斯(FW-H)进行的流动分析与FFOCS(FWH)方程进行了相似的音乐噪声与三个连接的巡航刀片相似传统的三刃螺旋桨,但大于传统的六刃螺旋桨。

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