反应性气膜对喷管附面层损失的影响

Qunli Cheng, Shuyuan Liu, Peipei Wang, Songqi Hu, Weimeng Zhang, Linlin Liu

科研成果: 期刊稿件文章同行评审

摘要

Aiming at the two-dimensional axisymmetric nozzle,the effect of reactive gas film of hydrogen and n-decane on the nozzle boundary layer loss was investigated by numerical simulation.For the two different injection materials,the boundary layer loss of nozzle under different injection ratios of 0%,0.47%,1.07% and 1.42% were analyzed and compared.The results show that the reactive gas film formed by the wall injection significantly reduces the nozzle wall temperature compared to the non-injection case. When the injection ratio increases from 0% to 1.42%,the hydrogen reactive gas film makes the average wall temperature of the nozzle expansion section reduced by 2648.3 K.However,the n-decane reactive gas film causes the average wall temperature of the nozzle expansion section to decrease by 1875.9 K.The n-decane injection is not beneficial to reduce the boundary layer loss of the nozzle, which increases the nozzle boundary layer loss by 504.3%.Meanwhile,hydrogen injection is conducive to reducing the nozzle boundary layer loss,which reduces the boundary layer loss by 38.8%.Therefore,the hydrogen reactive film is more beneficial to improve thermal protection and drag reduction of nozzle boundary layer.

投稿的翻译标题Influence of reactive gas film on nozzle boundary layer loss
源语言繁体中文
页(从-至)331-340
页数10
期刊Guti Huojian Jishu/Journal of Solid Rocket Technology
47
3
DOI
出版状态已出版 - 6月 2024

关键词

  • boundary layer loss
  • heat protection
  • nozzle
  • reactive gas film
  • rocket motor

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