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Study on flow and heat transfer characteristics of surface tension tank based on heat capacity method
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Lulu ZHAI1, Liang ZHANG1, Zuchao ZHU1, 2, Jintao LIU3, Wen LI3
Fluid Machinery | 2025, 53(10) : 94 - 101
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Fluid Machinery | 2025, 53(10): 94-101
Study on flow and heat transfer characteristics of surface tension tank based on heat capacity method
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Lulu ZHAI1, Liang ZHANG1, Zuchao ZHU1, 2, Jintao LIU3, Wen LI3
Affiliations
  • 1Zhejiang Key Laboratory of Multiflow and Fluid Machinery,Zhejiang Sci‑Tech University,Hangzhou 310018,China
  • 2Hefei General Machinery Research Institute Co.,Ltd.,Hefei 230031,China
  • 3Beijing Institute of Control Engineering,Beijing 100094,China
Published: 2025-10-31 doi: 10.3969/j.issn.1005-0329.2025.10.011
Outline
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To achieve accurate measurement of residual propellant in on‑orbit satellites,based on thermal‑fluid‑structure coupling calculation method,numerical calculations were conducted on the transient flow and heat transfer characteristics of propellant during heat capacity measurement.The flow characteristics,temperature distribution,and heat flux distribution characteristics of propellant in the tank under different settling acceleration conditions were analyzed.By comparing real‑time temperature change data from simulation and experimental monitoring points,the accuracy of the numerical calculation model was verified.The results show that the sloshing frequency of liquid propellant in the tank increases with increasing settling acceleration.When settling acceleration increases from 0.066 5 m/s2 to 0.294 m/s2,the propellant sloshing frequency increases from 0.055 Hz to 0.116 Hz.The temperature change of fluid above the gas‑liquid interface is more significant compared to that below the interface.After continuously heating the tank surface at 180 W total power for 180 seconds,there exists a certain temperature difference between the outer wall of the tank and the fluid‑structure interface,with an average temperature difference of 0.12 K.The lower the monitoring point position,the slower the temperature rises.The main frequency of temperature change at monitoring points inside the tank is consistent with the variation in liquid propellant sloshing frequency.The research results can provide references for the measurement of residual propellant quantity in on‑orbit satellites.

heat capacity method  /  surface tension tank  /  microgravity environment  /  propellant  /  flow characteristics  /  heat transfer characteristics
翟璐璐, 张梁, 朱祖超, 刘锦涛, 李文. 基于热容法的表面张力贮箱流动及传热特性研究. 流体机械, 2025 , 53 (10) : 94 -101 . DOI: 10.3969/j.issn.1005-0329.2025.10.011
Lulu ZHAI, Liang ZHANG, Zuchao ZHU, Jintao LIU, Wen LI. Study on flow and heat transfer characteristics of surface tension tank based on heat capacity method[J]. Fluid Machinery, 2025 , 53 (10) : 94 -101 . DOI: 10.3969/j.issn.1005-0329.2025.10.011
Year 2025 volume 53 Issue 10
77
24
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Article Info
doi: 10.3969/j.issn.1005-0329.2025.10.011
  • Receive Date:2025-02-18
  • Online Date:2026-10-20
  • Published:2025-10-31
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History
  • Received:2025-02-18
  • Revised:2025-07-27
Affiliations
    1Zhejiang Key Laboratory of Multiflow and Fluid Machinery,Zhejiang Sci‑Tech University,Hangzhou 310018,China
    2Hefei General Machinery Research Institute Co.,Ltd.,Hefei 230031,China
    3Beijing Institute of Control Engineering,Beijing 100094,China
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表12种不同金属材料的力学参数
科
Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)
属
Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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