Numerical simulation of hypersonic inlet flows with equilibrium or finite rate chemistry

Author(s):  
SHENG-TAO YU ◽  
KWANG-CHUNG HSIEH ◽  
JIAN-SHUN SHUEN ◽  
BONNIEJ. MCBRIDE
1998 ◽  
Author(s):  
J. van Keuk ◽  
J. Ballmann ◽  
A. Schneider ◽  
W. Koschel

1986 ◽  
Vol 2 (4) ◽  
pp. 381-382 ◽  
Author(s):  
Wing-Fai Ng ◽  
Thomas J. Benson ◽  
William G. Kunik

2013 ◽  
Vol 482 ◽  
pp. 375-380
Author(s):  
Hong Ming Zhang ◽  
Li Xiang Zhang

The paper presents the re-entrant jet analysis of cavitating turbulent flow on a hydrofoil. Analysis was performed by OpenFOAM code. A mixture assumption and a finite rate mass transfer model were introduced. The finite volume method is used to solve the governing equations of the mixture model and the pressure-velocity coupling is handled via a Pressure Implicit with Splitting of Operators (PISO) procedure. The result of numerical simulation clearly explained the mechanism of re-entrant jet and quasi-periodic law of cavitating flow on a hydrofoil.


2013 ◽  
Vol 291-294 ◽  
pp. 1958-1962 ◽  
Author(s):  
Hong Ming Zhang ◽  
Li Xiang Zhang

The paper presents numerical simulation of blade channel vortex in a low head Francis turbine using OpenFoam code. A mixture assumption and a finite rate mass transfer model were introduced to analyze blade channel vortex. The finite volume method is used to solve the governing equations of the mixture model and the pressure-velocity coupling is handled via a Pressure Implicit with Splitting of Operators (PISO) procedure. Simulation results have shown that using cavitation model to analyze blade channel vortex is very effective.


2011 ◽  
Vol 4 (4) ◽  
pp. 89-103
Author(s):  
Juan-Camilo Lezcano-Benítez ◽  
Daniel Correa-Restrepo ◽  
Andrés-Adolfo Amell-Arrieta ◽  
Francisco-Javier Cadavid-Sierra

In this paper we present the results of a 2D‑axisymmetric parametric study which simulates an atmospheric premixed burner with flame at high pressure, in which methane is burned. A total of 9 simulations are performed with different regulators openings of primary and secondary air. Also, it provides a 3D simulation in which entry conditions are the profiles obtained in a 2D‑axisymmetric simulation, with the intention to note that differences are obtained between 2D and 3D simulation. The simulations are performed using the standard k-ε model for turbulence, P1 model for radiation and the Finite Rate/Eddy Dissipation model with a simplified 2-step reaction mechanism for combustion. We conclude that when the secondary air regulator is closed, combustion is incomplete. Also, the results of 2D‑axisymmetric are a good approximation in regards to 3D results.


1992 ◽  
Vol 29 (6) ◽  
pp. 1049-1056 ◽  
Author(s):  
Yasuhiro Wada ◽  
Hirotoshi Kubota

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