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86                                          真空与低温                                   第 32 卷 第  1  期


              现象。                                                  ized liquid hydrogen tanks[J]. International Journal of Hydro-
                  (3)从对流换热功率的角度来分析,变重力下                            gen Energy,2022,47(71):30530−30545.
              液相与壁面对流换热功率仍远高于气相。超重力                             [7]   SEO M,JEONG S. Analysis of self-pressurization phenome-
              至微重力过渡阶段,换热功率明显降低,且重力加                               non  of  cryogenic  fluid  storage  tank  with  thermal  diffusion
              速度越接近零,功率最小值越趋近零;微重力恢复                               model[J]. Cryogenics,2010,50(9):549−555.
                                                                [8]   HASTINGS  L  J, FLACHBART  R  H, MARTIN  J  J, et  al.
              至常重力阶段,气液相与壁面换热功率瞬间大幅增
                                                                   Spray bar zero-gravity vent system for on-orbit liquid hydro-
              长后回落至常重力水平,且重力加速度越接近零波
                                                                   gen storage[R]. NASA/TM-2003-212926,2003.
              动幅度越大,是造成压力与温度也随之变化的可能
                                                                [9]   KASSEMI M,HYLTON S,KARTUZOVA O V,et al. Sharp
              原因。
                                                                   interface  CFD  analysis  of  a  liquid  methane  self-pressuriza-
              参考文献:                                                tion  experiment  in  1G  and  microgravity[C]//AIAA  Scitech
                                                                   2025 Forum,2025.
              [1]   LIN C,HASAN M. Self-pressurization of a spherical liquid  [10]   王夕,王珏,容易,等. 微重力下低温贮箱内推进剂相变仿
                 hydrogen  storage  tank  in  a  micro  gravity  environment[C]//  真模型研究  [J]. 导弹与航天运载技术,2018(1):36−40.
                 Proceedings of the 30th Aerospace Sciences Meeting and Ex-  [11]   刘展,孙培杰,李鹏,等. 微重力下低温液氧贮箱热分层研
                 hibit. Reno,Nevada,United States,January 6-9,1992.  究  [J]. 低温工程,2016(1):25−31.
              [2]   ESTEY P N,LEWIS D H J,CONNOR M. Prediction of a  [12]   MAJUMDAR  A, VALENZUELA  J, LECLAIR  A, et  al.
                 propellant tank pressure history using state space methods[J].  Numerical modeling of self-pressurization and pressure con-
                 Journal of Spacecraft and Rockets,1983,20(1):49−54.  trol by a thermodynamic vent system in a cryogenic tank[J].
              [3]   BAILEY  T, VANDEKOPPEL  R, SKARTVEDT  G, et  al.  Cryogenics,2016,74:113−122.
                 Cryogenic propellant stratification analysis and test data cor-  [13]   BELL I H,WRONSKI J,QUOILIN S,et al. Pure and pseu-
                 relation[J]. AIAA Journal,1963,1(7):1657−1659.     do-pure  fluid  thermophysical  property  evaluation  and  the
              [4]   BAILEY T E,FEARN R F. Analytical and experimental de-  open-source  thermophysical  property  library  CoolProp[J].
                                                                    Industrial & Engineering Chemistry Research,2014,53(6):
                 termination of liquid-hydrogen temperature stratification[C]//
                 Advances in Cryogenic Engineering:Proceedings of the 1963  2498−2508.
                 Cryogenic Engineering Conference ,Colorado Boston,MA.  [14]   SCHMIDT F W,HENDERSON R E,WOLGEMUTH C H.
                                                                    Introduction  to  thermal  sciences(2nd  ed)[M].  New  York:
                 August 19–21,1963.
                                                                    John Wiley & Sons,1993.
              [5]   DAIGLE M J,NAPLES A,HURT J,et al. Temperature strat-
                                                                [15]   MAZUMDER S. Numerical methods for partial differential
                 ification  in  a  cryogenic  fuel  tank[J].  Journal  of  Thermo-
                                                                    equations:Finite difference and finite volume methods[M].
                 physics and Heat Transfer,2013,27(1):116−126.
                                                                    Academic Press,2015.
              [6]   WANG H R,WANG B,PAN Q W,et al. Modeling and ther-
                 modynamic analysis of thermal performance in self-pressur-            (责任编辑:杨建斌)















              引文信息:毛若曈,黄永华,高翔宇,等. 变重力条件下低温推进剂贮箱自增压与热分层建模及其特性研究[J]. 真空与低温,
                      2026,32(1):77−86.
                      MAO R T,HUANG Y H,GAO X Y,et al. Modeling and analysis of self-pressurization and thermal stratification in cryo-
                      genic propellant tanks under variable gravity[J]. Vacuum and Cryogenics,2026,32(1):77−86.
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