• DocumentCode
    2929326
  • Title

    Numerical Simulation of Two Phase Flow with Evaporation in Supersonic Cross Flow

  • Author

    Rui Shou-zhen ; Xing Yu-ming

  • Author_Institution
    Sch. of Aeronaut. Sci. & Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
  • fYear
    2011
  • fDate
    25-28 March 2011
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    Spraying water into high temperature high pressure gas is a two phase flow. An Euler-Lagrange method was used to simulate the two phase flow with evaporation. The gas phase is simulated by solving the Navier-Stokes equations using RK(Runge-Kutta)-AUSM+(Advection Upstream Splitting Method) scheme. A particle trajectory model was used to represent the liquid phase. The source terms were added to the gas phase conservation equations to simulate the couple of the two phases. Several applications are calculated to analyze the droplet evaporation and the influence on gas flow field and energy output. The conclusions are useful for the gas-steam launching system and energy regulation design and optimization.
  • Keywords
    Navier-Stokes equations; Runge-Kutta methods; computational fluid dynamics; evaporation; steam; supersonic flow; two-phase flow; Euler-Lagrange method; Navier-Stokes equation; Runge-Kutta-AUSM method; advection upstream splitting method; energy regulation design; evaporation; gas flow field; gas-steam launching system; high temperature high pressure gas; particle trajectory model; supersonic cross flow; two phase flow; water spraying; Equations; Mathematical model; Numerical models; Numerical simulation; Orifices; Temperature; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power and Energy Engineering Conference (APPEEC), 2011 Asia-Pacific
  • Conference_Location
    Wuhan
  • ISSN
    2157-4839
  • Print_ISBN
    978-1-4244-6253-7
  • Type

    conf

  • DOI
    10.1109/APPEEC.2011.5748511
  • Filename
    5748511