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开孔壁蜂窝器整流特性实验研究

符澄 彭强 李毅 廖达雄 吕金磊 朱博

实验流体力学2016,Vol.30Issue(5):17-22,6.
实验流体力学2016,Vol.30Issue(5):17-22,6.DOI:10.11729/syltlx20150111

开孔壁蜂窝器整流特性实验研究

Experimental study of flow straightening and turbulence reduction characteristics for porosity honeycomb

符澄 1彭强 2李毅 3廖达雄 3吕金磊 1朱博1

作者信息

  • 1. 中国空气动力研究与发展中心 空气动力学国家重点实验室,四川 绵阳 621000
  • 2. 中国空气动力研究与发展中心 设备设计及测试技术研究所,四川 绵阳 621000
  • 3. 中国空气动力研究与发展中心 设备设计及测试技术研究所,四川 绵阳 621000
  • 折叠

摘要

Abstract

The honeycomb is an important device which is installed in wind tunnel settling chamber to improve the flow uniformity and decrease the flow angle as well as the turbulence in-tensity in the wind tunnel test section.For a regular honeycomb,in order to improve the flow straightening and turbulence reduction characteristics,a large length-diameter ratio must be used in the design of the honeycomb which results in the increase of total pressure loss of the ho-neycomb.A new type of honeycomb with a group of small holes on the wall of honeycomb cells is designed.This type of porosity honeycomb can achieve the exchange of the vortices and pressure between different cells to significantly improve the flow quality downstream the honeycomb.In the solid wall test section of the 0.55m×0.40m low noise aeronautic acoustic wind tunnel,the 2D hot wire is used to measure the turbulence intensity and velocity distribution downstream the porosity honeycomb and the regular one respectively with different flow velocities.The experi-mental results indicate that the honeycomb with 50% transverse porosity can reduce the turbu-lence intensity by 13.8% compared against the regular one.The velocity distribution downstream the honeycomb becomes smoother and the flow angle is also reduced.The design of the flow straightening and turbulence reduction system for the wind tunnel with the optimized porosity ho-neycomb can reduce the number of screens or the constriction ratio of the wind tunnel,and there-fore,reduce the power consumption and the construction budget of wind tunnels.

关键词

风洞/蜂窝器/流场品质/湍流度/气流偏角/热线风速仪

Key words

wind tunnel/honeycomb/flow quality/turbulence intensity/flow angularity/hot wire

分类

航空航天

引用本文复制引用

符澄,彭强,李毅,廖达雄,吕金磊,朱博..开孔壁蜂窝器整流特性实验研究[J].实验流体力学,2016,30(5):17-22,6.

基金项目

空气动力学国家重点实验室基金资助(SKLA-2012-04-03) (SKLA-2012-04-03)

实验流体力学

OA北大核心CSCDCSTPCD

1672-9897

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