墨西哥国立大学墨西哥边界层风洞特征及标定

Edmundo Amaya Gallardo, Adrián Pozos Estrada, R. Gómez Martínez
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引用次数: 1

摘要

为了改进和促进墨西哥风工程研究,在墨西哥国立自治大学(UNAM)建立了一个用于大气环境和结构风荷载模拟的低速闭式回风洞。测试校准程序是根据几位作者在文献中指定的许多建议制定的,以确保符合全尺寸测量、实验室结果和国际编码。校正过程包括四个阶段:第一阶段是充分表示大气边界层;第二,获得足够的刚性模型压力系数;第三,进行试验,从结构模型中获得气动力和一些动力特性;第四是发展气动弹性模型。本文主要研究前两个阶段。因此,在第一阶段,开发了各种任务,以便对大气边界层下部进行充分的表征,以表征平均速度剖面和湍流波动。在第二阶段,主要任务是复制典型立方体低层建筑的外部平均压力系数,正如许多其他实验室之前所做的那样。在第一阶段,有可能人工地充分复制城市大气边界层。在第二阶段,一些结果表明需要更新当前墨西哥的风力设计法规,因为一些压力系数大大超过了阈值。最后,尽管其他类型的试验正在进行中,但认为该新边界层风洞可以放心地用于测试不同类型的结构,并为墨西哥风工程的发展做出贡献。
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Characteristics and calibration of the mexican boundary layer wind tunnel at UNAM
With the aim to improve and promote Mexican Wind Engineering research, a low-speed closed return wind tunnel for atmospheric environment and structural wind-loading simulations was built at the National Autonomous University of Mexico (UNAM). The testing calibration procedure was developed based on many recommendations specified by several authors on the literature to assure compliance with full-scale measurements, laboratory results and international coding. The calibration procedure consists of four stages: the first stage is to represent adequately the atmospheric boundary layer; the second, to obtain adequate pressure coefficients for rigid models; the third, to perform tests to obtain the aerodynamic forces and some dynamic properties from structural models; and the fourth is to develop aeroelastic models. This paper focuses on the first two stages. Therefore, during the first stage, various tasks were developed to perform adequate representation on the lower-portion of the atmospheric boundary layer to characterize mean velocity profiles and turbulence fluctuations. On the second stage, the main task was to replicate external mean pressure coefficients of a typical cubic low-rise building as many other laboratories have done before. During the first stage it was possible to adequately replicate an urban atmospheric boundary layer artificially. During the second stage, some results reveal the need to update the current Mexican regulations for wind design, since some pressure coefficients considerably exceeds the threshold values. Finally, although other types of tests are in progress, it is considered that the new boundary layer wind tunnel of the UNAM can be used with confidence to test different type of structures and contribute to the development of Mexican Wind Engineering.
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审稿时长
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