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固体推进剂燃烧中凝相粒子的激光全息测试 被引量:11

Laser Holographic Measurement of Condensed Phase Particles during Solid Propellant Combustion
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摘要 概述了测试凝相粒子尺寸的基本方法 ,较详细地阐述了研究燃烧场凝相粒子尺寸分布的激光全息测量方法和测试结果。 Some basic methods of measuring condensed phase particle size are summarized. The laser holographic measuring method and some measured results of the condensed phase particle size distribution in the investigation of combustion flow field are presented in detail.
出处 《固体火箭技术》 EI CAS CSCD 2000年第1期70-73,共4页 Journal of Solid Rocket Technology
基金 国防科技重点实验室基金
关键词 激光全息测试 固体推进剂燃烧 凝相粒子 laser holographic imaging aluminized propellant propellant combustion
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参考文献5

  • 1[1]George D. Recent advances in solid rocket motor performance prediction capacity [R]. AIAA81-0033,1981.
  • 2[2]Koo J H. A review of particle sizing methods in rocket propulsion [R]. AD/AI190163.
  • 3[3]Sang Chu Yoon. Holography investigation of solid propellant combustion in a three-dimensional motor [R]. ADA164217.
  • 4[4]Thomas R G. Holographic investigation of solid propellant particulate [R]. ADA112748.
  • 5[5]Brennan W D. et al. Measured particulate behavior in a subscale solid propellant rocket motor [J]. Journal of Propulsion and Power, Vol.8.No.5.Sept-oct.

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