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
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