节点文献

低(变)湍流度风洞设计再探讨

The further research on the design of low (varying) turbulence wind tunnel

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 侯志勇王连泽周建和何克敏

【Author】 HOU Zhi-yong1,WANG Lian-ze2,ZHOU Jian-he3,HE Ke-min4(1.Department of Space Equipment,the Academy of Equipment Command & Technology,Beijing 101416,China;2.School of Aerospace,Tsinghua University,Beijing 100084,China;3.Tianjin University,Tianjin 300072,China;4.Northwestern Polytechnical University,Xi’an 710072,China)

【机构】 装备指挥技术学院航天装备系清华大学航天航空学院天津大学西北工业大学

【摘要】 在资料调研与总结国内约20年来成功研制低(变)湍流度风洞的基础上,介绍了这类风洞设计思想中几点有新意的方法,供设计者参考。对减湍起决定作用的稳定段布局设计给出了一组综合性图线;对减湍起重要作用的收缩段设计提出了通用便捷的方法;对全系统起优化作用的风扇动力段及拐角导流片设计研制等有一定的新见解。

【Abstract】 Based on intensive investigation and successfully constructed wind tunnels in the past twenty years,the paper reviews some new ideas on the low(varying) turbulence wind tunnel design and they can be reference for engineering design.The paper gives the integrative curve for the design of stable section which plays a crucial role in reducing turbulence intensity,and the universal method for the contraction section which plays an important role in reducing turbulence intensity.Also it is proposed some personal opinion on the design of the power section and turning deflector,which optimize the whole system.

  • 【文献出处】 实验流体力学 ,Journal of Experiments in Fluid Mechanics , 编辑部邮箱 ,2011年01期
  • 【分类号】V211.74
  • 【被引频次】22
  • 【下载频次】586
节点文献中: 

本文链接的文献网络图示:

本文的引文网络