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气动加热影响下的液氧储罐内温度分层与相变特性仿真分析

汪艳 孙培杰 耑锐 匡以武 王文

南京航空航天大学学报2017,Vol.49Issue(6):845-850,6.
南京航空航天大学学报2017,Vol.49Issue(6):845-850,6.DOI:10.16356/j.1005-2615.2017.06.014

气动加热影响下的液氧储罐内温度分层与相变特性仿真分析

Temperature Stratification and Phase Transition in Liquid Oxygen Tank with Aerodynamic Heating Boundary

汪艳 1孙培杰 2耑锐 2匡以武 1王文1

作者信息

  • 1. 上海交通大学制冷与低温工程研究所 ,上海 ,200240
  • 2. 上海宇航系统工程研究所 ,上海 ,201108
  • 折叠

摘要

Abstract

Pre-pressurization rise process of the liquid oxygen stored in a tank is simulated through 3D CFD simulations . The phase transformation rate and temperature stratification of liquid oxygen are specified . The results suggest that evaporation rate of the liquid oxygen is fluctuating around 0 .0126 kg/s under the aerodynamic heating boundary condition .The liquid oxygen boiling rate near the wall is also investigated and averagely reaches 0 .086 kg/s in the whole process ,which is consistent with the tank heat leakage .The temperature stratification is observed when the high-temperature gas pres-surization enters the tank by a diffuser .The liquid oxygen temperature in the gas-liquid interface increa-ses from 89 .51 K to 93 .61 K .The average increasing rate of the liquid temperature is 0 .022 K/s for 183 s after the pre-pressurization .

关键词

液氧储箱/气动加热/蒸发和沸腾速率/温度分层

Key words

liquid oxygen tank/aerodynamic heating/evaporation and boiling rate/temperature stratifica-tion

分类

航空航天

引用本文复制引用

汪艳,孙培杰,耑锐,匡以武,王文..气动加热影响下的液氧储罐内温度分层与相变特性仿真分析[J].南京航空航天大学学报,2017,49(6):845-850,6.

基金项目

上海航天SAST基金(SAST201414)资助项目. (SAST201414)

南京航空航天大学学报

OA北大核心CSCDCSTPCD

1005-2615

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