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Experimental investigation on heat flux measurement of nozzle throat

  • Hu Liang Xiao
  • , Chun Bo Hu
  • , Sheng Min Zhang
  • , Zhe Deng
  • , Fei Qin
  • Northwestern Polytechnical University Xian

科研成果: 期刊稿件文章同行评审

3 引用 (Scopus)

摘要

In order to isolate the effect of thermochemistry ablation on measuring the heat flux of nozzle throat, the experiments were carried out by using a HT50-20 heat flux transducer to obtain the heat flux density in nozzle throat under various incoming flow conditions as well as the parameters of the burning gases. Meanwhile, on the basis of experiments, numerical simulation was conducted to investigate the heat flux of nozzle throat. The experimental results show that the heat flux density is 0.496 MW/m2, 0.471 MW/m2, 0.317 MW/m2 when the temperature of burning gases at the nozzle throat is 611 K, 551 K, 457 K respectively. Furthermore, the data of experiments can be used to validate the numerical simulation.

源语言英语
页(从-至)138-142
页数5
期刊Guti Huojian Jishu/Journal of Solid Rocket Technology
36
1
DOI
出版状态已出版 - 2月 2013

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