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中国沙漠 ›› 1998, Vol. 18 ›› Issue (4): 334-339.

• 研究论文 • 上一篇    下一篇

室内沙风洞空洞条件下流场规律

郝青振, 邹学勇, 董光荣, 李长治, 王国昌   

  1. 中国科学院兰州沙漠研究所, 兰州 730000
  • 收稿日期:1997-12-23 修回日期:1990-05-19 出版日期:1998-12-20 发布日期:1998-12-20
  • 作者简介:郝青振,男,1971年生,理学硕士研究生。研究方向风沙物理与沙漠环境。
  • 基金资助:
    中科院重大项目(KZ951-B1-206)资助

THE FLOW FIELD LAW UNDER EMPTY TUNNEL CONDITION IN INDOOR WIND TUNNEL

HAO Qing zhen, ZOU Xue yong, DONG Guang rong, LI Chang zhi, WANG Guo chang   

  1. Institute of Desert Research, Chinese Acadamy of Sciences, Lanzhou 730000
  • Received:1997-12-23 Revised:1990-05-19 Online:1998-12-20 Published:1998-12-20

摘要: 根据中国科学院兰州沙漠研究所室内沙风洞空洞条件下的气流场测定结果,阐述了风洞实验段内边界层发展、气流加速、底板边界层内的风速分布、自由流区风速不均匀性等规律,其中底板边界层内的风速分布遵循Coles定律和指数定律,不完全遵循普兰特-冯·卡曼对数定律。

关键词: 空洞, 边界层, 流场规律

Abstract: Flow field visualization test is one of important contents in wind tunnel experiment. Limited by similar conditions, the flow field measurement of modles about dunes or sand preventing engineerings may not be conducted under sand holding condition. So, there is most significance to proclaim flow field law under empty tunnel for programme's design and result's calibration. The experiment is conducted in the famous indoor wind tunnel of Lanzhou Desert Research Institute. The total length of the tunnel is 3778 m, in which that of working section is 1623 m. Its cross section has 10 m width and 06 m height. Wind velocity can be regulated from 2 m/s to 40 m/s, and turbulency is less than 0.4% in the tunnel. There are five groups of wind velocity including 60,80,100,120 and 140 m/s are tested. Between the section of 33-141 m, there are eight cross sections at 35,55,75,90,10.5,120,135 and 145 respectively. All sixty three measurement points distribute within the right part of cross sections and 0-03 m over the bottom floor. The studing results prove that the isogram of wind velocity in whole cross sections looks like butterfly; the wind velocity distribution in boundary layer of bottom floor obeys exponent law, and the coefficient (d) of wind velocity increasing along the axis can be expressed as d=0062x 0.431; the development of boundary layer over bottom floor follows a formula of δ=3046x 0.676. According to the study, it is suggested that experiment model should be located between 10 and 140 m in working section, and 01 m away from lateral wall of the tunnel; the testing wind velocity should be controlled within 20 m/s.

Key words: Empty tunnle, Boundary layer, Flow field law

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