Skip to main content
Log in

Effect of External Heat Input on Fluid Sloshing Dynamic Performance in a Liquid Oxygen Tank

  • Original Paper
  • Published:
International Journal of Aeronautical and Space Sciences Aims and scope Submit manuscript

Abstract

In the present study, a numerical model is developed to research the effect of the heat input on fluid sloshing. The volume of fluid method is used to simulate fluid reciprocating motion during sloshing with the mesh motion treatment being coupled. The external sloshing excitation is realized by user-defined functions and the convection thermal boundary condition is adopted to consider the heat exchange between the tank and the external environment. The model validation is made with the relative error being less than five percent. Based on the developed numerical model, the variation of fluid pressure, interface fluctuation, fluid sloshing hydrodynamics and fluid temperature distribution are, respectively, analyzed. Some conclusions are obtained finally. The present study is significant to the fluid sloshing suppression in cryogenic fuel storage tanks.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12

Similar content being viewed by others

References

  1. Peterson LD, Crawley EF, Hansman RJ (1989) Nonlinear fluid slosh coupled to the dynamics of a spacecraft. AIAA J 9(27):1230–1240

    Article  Google Scholar 

  2. Modaressi-Tehrani K, Rakheja S, Stiharu I (2007) Three-dimensional analysis of transient slosh within a partly-filled tank equipped with baffles. Veh Syst Dyn 6(45):525–548

    Article  Google Scholar 

  3. Reyhanoglu M, Hervas JR (2012) Nonlinear dynamics and control of space vehicles with multiple fuel slosh modes. Control Eng Pract 9(20):912–918

    Article  Google Scholar 

  4. Ludwig C, Dreyer ME, Hopfinger EJ (2013) Pressure variations in a cryogenic liquid storage tank subjected to periodic excitations. Int J Heat Mass Transf 66:223–234

    Article  Google Scholar 

  5. Kolaei A, Rakheja S, Richard MJ (2014) Range of applicability of the linear fluid slosh theory for predicting transient lateral slosh and roll stability of tank vehicles. J Sound Vib 1(333):263–282

    Article  Google Scholar 

  6. Cho IH, Kim MH (2016) Effect of dual vertical porous baffles on sloshing reduction in a swaying rectangular tank. Ocean Eng 126:364–373

    Article  Google Scholar 

  7. Chiba M, Magata H (2017) Influence of liquid sloshing on dynamics of flexible space structures. J Sound Vib 401:1–22

    Article  Google Scholar 

  8. Grotle EL, Bihs H, Æsøy V (2017) Experimental and numerical investigation of sloshing under roll excitation at shallow liquid depths. Ocean Eng 138:73–85

    Article  Google Scholar 

  9. Liu Z, Feng Y, Lei G, Li Y (2019) Sloshing behavior under different initial liquid temperatures in a cryogenic fuel tank. J Low Temp Phys 196:347–363

    Article  Google Scholar 

  10. Liu Z, Feng Y, Lei G, Li Y (2019) Hydrodynamic performance in a sloshing liquid oxygen tank under different initial liquid filling levels. Aerosp Sci Technol 85:544–555

    Article  Google Scholar 

  11. Liu Z, Feng Y, Lei G, Li Y (2019) Fluid sloshing dynamic performance in a liquid hydrogen tank. Int J Hydrog Energy 44(26):13885–13894

    Article  Google Scholar 

  12. Liu Z, Feng Y, Cui J, Lei G, Li Y (2019) Effect of excitation types on sloshing dynamic characteristics in a cryogenic liquid oxygen tank. J Aerosp Eng 32(6):04019096

    Article  Google Scholar 

  13. Denner F, vanWachem BGM (2019) Numerical modelling of shock-bubble interactions using a pressure-based algorithm without Riemann solvers. Exp Comput Multiph Flow 1(4):271–285

    Article  Google Scholar 

  14. Liu Z, Li Y, Jin Y (2016) Pressurization performance and temperature stratification in cryogenic final stage propellant tank. Appl Therm Eng 106:211–220

    Article  Google Scholar 

  15. Liu Z, Li Y, Jin Y, Li C (2017) Thermodynamic performance of pre-pressurization in a cryogenic tank. Appl Therm Eng 112:801–810

    Article  Google Scholar 

  16. Liu Z, Li C (2018) Influence of slosh baffles on thermodynamic performance in liquid hydrogen tank. J Hazard Mater 346:253–262

    Article  Google Scholar 

  17. Liu Z, Li Y, Zhou G (2018) Study on thermal stratification in liquid hydrogen tank under different gravity levels. Int J Hydrog Energy 19(43):9369–9378

    Article  Google Scholar 

  18. Gu X, Wen J, Tian J, Li C, Liu H, Wang S (2019) Role of gravity in condensation flow of R1234ze (E) inside horizontal mini/macro-channels. Exp Comput Multiph Flow 1(3):219–229

    Article  Google Scholar 

  19. Yang Z, Peng XF, Ye P (2008) Numerical and experimental investigation of two phase flow during boiling in a coiled tube. Int J Heat Mass Transf 51:1003–1016

    Article  Google Scholar 

  20. NIST, Chemistry, Web Book, NIST Standard Reference Database Number 69, (October 2011 Release), 2011 http://webbook.nist.gov/chemistry/

  21. Faghri A, Zhang Y, Howell JR (2010), Advanced heat and mass transfer, Global Digital Press

  22. Grotle EL, Æsøy V (2018) Dynamic modelling of the thermal response enhanced by sloshing in marine LNG fuel tanks. Appl Therm Eng 135:512–520

    Article  Google Scholar 

Download references

Acknowledgements

This work was supported by the Fundamental Research Funds for the Central Universities (2019GF11).

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Zhan Liu.

Additional information

Publisher's Note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Liu, Z., Feng, Y., Liu, Y. et al. Effect of External Heat Input on Fluid Sloshing Dynamic Performance in a Liquid Oxygen Tank. Int. J. Aeronaut. Space Sci. 21, 879–888 (2020). https://doi.org/10.1007/s42405-020-00261-y

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s42405-020-00261-y

Keywords

Navigation