反应性气膜对喷管附面层损失的影响

Translated title of the contribution: Influence of reactive gas film on nozzle boundary layer loss

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

Research output: Contribution to journalArticlepeer-review

Abstract

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.

Translated title of the contributionInfluence of reactive gas film on nozzle boundary layer loss
Original languageChinese (Traditional)
Pages (from-to)331-340
Number of pages10
JournalGuti Huojian Jishu/Journal of Solid Rocket Technology
Volume47
Issue number3
DOIs
StatePublished - Jun 2024

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