在科隆DNW-KKK低温风洞中进行车辆空气动力学试验

W. Becker, R. Rebstock, S. Loose, H. Richard, M. Raffel
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引用次数: 2

摘要

随着新一代高速列车速度的不断提高,其几何结构变得越来越重要,气动设计也必须得到更详细的考虑。特别是火车的侧风敏感性本质上是一个问题,必须相应地加以考虑。早先通过粒子图像测速(PIV)在较小的风洞中进行的测量显示,在模型的背风侧存在一个强涡。为了解决这一问题,在通用高速列车模型上进行了PIV测试和力测量。模型的比例因子为1:10。外形和几何比例几乎与德国ICE1列车相似。为了研究低温科隆风洞(KKK)的力和扭矩数据,将ice模型应用于半模型平衡。本文给出了这些结果。边界层厚度是影响测量结果的重要参数。在半跨模型试验中,采用支架与机身之间的隔梁解决了这一问题。改变模型与地平面的距离,以确定其对ice模型测量的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Tests for vehicle aerodynamics in the cryogenic wind tunnel Cologne DNW-KKK
With the increasing speed of new generations of high speed trains their geometry is becoming increasingly important and the aerodynamic design has to be considered in greater detail. Particularly the train's crosswind sensitivity is a problematic in nature and has to be considered accordingly. Earlier measurements by means of particle image velocimetry (PIV) in smaller wind tunnels showed the presence of a strong vortex at the leeward side of the model. To address this issue, PIV tests and also force measurement were made on a generic high speed train model. The scaling factor of the model was 1:10. Contour and geometric ratios are nearly similar to the German ICE1 train. For the investigation of force and torque data the ICE-Model was adapted to the half model-balance of cryogenic wind tunnel Cologne (KKK). These results are presented herein. The boundary layer thickness is an essential parameter influencing the measurements. In case of semi-span model tests this problem is solved by using a peniche (standoff) between support and fuselage. The model-ground plane distance was varied in order to determine it's influence on the ICE-model measurements.
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