期刊文献+

Numerical investigation on characteristics of interfacial wave of liquid film in gas-liquid two-phase flow using OpenFOAM 被引量:1

原文传递
导出
摘要 Liquid film cooling as an advanced cooling technology is widely used in space vehicles.Stable operation of liquid film along the rocket combustion inner wall is crucial for thermal protection of rocket engines.The stability of liquid film is mainly determined by the characteristics of interfacial wave,which is rarely investigated right now.How to improve the stability of thin film has become a hot spot.In view of this,an advanced model based on the conventional Volume of Fluid(VOF)model is adopted to investigate the characteristics of interfacial wave in gas-liquid flow by using OpenFOAM,and the mechanism of formation and development of wave is revealed intuitively through numerical study.The effects from gas velocity,surface tension and dynamic viscosity of liquid(three factors)on the wave are studied respectively.It can be found that the gas velocity is critical to the formation and development of wave,and four modes of droplets generation are illustrated in this paper.Besides,a gas vortex near the gas-liquid interface can induce formation of wave easily,so changing the gas vortex state can regulate formation and development of wave.What’s more,the change rules of three factors influencing on the interfacial wave are obtained,and the surface tension has a negative effect on the formation and development of wave only when the surface tension coefficient is above the critical value,whereas the dynamic viscosity has a positive effect in this process.Lastly,the maximum height and maximum slope angle of wave will level off as the gas velocity increases.Meanwhile,the maximum slope angle of wave is usually no more than 38°,no matter what happens to the three factors.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2024年第2期233-248,共16页 中国航空学报(英文版)
  • 相关文献

参考文献1

二级参考文献57

  • 1Theofilis V. Global linear instability. Annu Rev Fluid Mech 2011;43:319-52.
  • 2Gomez F, Clainche SL, Paredes P, Hermanns M, Theofilis V. Four decades of studying global linear instability: progress and challenges. AIAA J 2012;50(12):2731-43.
  • 3Palacios F, Colonno MR, Aranake AC, Campos A, Copeland SR, Economon TD, et al. Stanford University unstructured (SU2): An open-source integrated computational environment for multiphysics simulation and design. Reston: AIAA; 2013. Report No.: AIAA- 2013-0287.
  • 4Fischer PF. An overlapping schwarz method for spectral element solution of the incompressible Navier-Stokes equations. J Comput Phys 1997;133(1):84-101.
  • 5Vos PE, Sherwin S J, Kirby RM. From h to p efficiently: Implementing finite and spectral hp element methods to achieve optimal performance for low-and high-order discretisations. J Comput Phys 2010;229(13):5161- 81.
  • 6Cantwell C, Sherwin S, Kirby R, Kelly P. From h to p efficiently: Strategy selection for operator evaluation on hexahedral and tetrahedral elements. Comput Fluids 2011 ;43(1):23 -8.
  • 7Weller HG, Tabor G, Jasak H, Fureby C. A tensorial approach to computational continuum mechanics using object-oriented tech- niques. Comput Phys 1998;12(6):620-31.
  • 8Tezuka A, Suzuki K. Three-dimensional global linear stability analysis of flow around a spheroid. AIAA J 2006;44(8):1697 -708.
  • 9Bagheri S, Schlatter P, Schmid P J, Henningson DS. Global stability of a jet in crossflow. J Fluid Mech 2009;624:33-44.
  • 10Gomez F, Gomez R, Theofilis V. On three-dimensional global linear instability analysis of flows with standard aerodynamics codes. Aerosp Sci Technol 2014;32(1):223 -34.

共引文献2

同被引文献6

引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部