首页> 美国政府科技报告 >Particle Flow within a Transonic Compressor Rotor Passage with Application to Laser-Doppler Velocimetry
【24h】

Particle Flow within a Transonic Compressor Rotor Passage with Application to Laser-Doppler Velocimetry

机译:跨声速压缩机转子通道内的粒子流与激光多普勒测速技术的应用

获取原文

摘要

A theoretical analysis was conducted of the dynamic behavior of micron size particles moving in the three-dimensional flow field of a rotating transonic axial-flow air compressor rotor. The particle velocity lag and angular deviation relative to the gas were determined as functions of particle diameter, mass density and radial position. Particle size and density were varied over ranges selected to correspond to typical laser-Doppler velocimeter (LDV) flow field mapping applications. It was found that the particles move essentially on gas stream surfaces and that particle tracking is relatively insensitive to the rotor radial coordinate. Velocity lag and angular deviation increased whenever particle size or mass density increased, and particle tracking was more sensitive to a change in particle diameter than to a corresponding change in mass density. Results indicated that velocity and angular deviations generally less than 1 percent and 1 degree could be achieved with 1 gm/cc tracer particles with diameters of 1 micron or less. (Author)

著录项

  • 作者

    Maxwell, B. R.;

  • 作者单位
  • 年度 1975
  • 页码 1-64
  • 总页数 64
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号