30th Joint Propulsion Conference and Exhibit 1994
DOI: 10.2514/6.1994-3329
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Numerical Simulation of Combustion Process in Rocket Combustion Chambers With Coaxial Injectors

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Cited by 5 publications
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“…All geometric transformations were performed in a CAD program, and grids were created in a CFD program. Aerodynamic studies of these devices were carried out according to the known methodology [17]. The standard k-ε model was used for research, which is one of the most widely used turbulence models due to its simplicity in modeling the structure of turbulent flows.…”
Section: Methodsmentioning
confidence: 99%
“…All geometric transformations were performed in a CAD program, and grids were created in a CFD program. Aerodynamic studies of these devices were carried out according to the known methodology [17]. The standard k-ε model was used for research, which is one of the most widely used turbulence models due to its simplicity in modeling the structure of turbulent flows.…”
Section: Methodsmentioning
confidence: 99%
“…The fluxes across the cell interface are computed by using a Riemann solver with min-mod limiter to limit the fluxes across the interface. The salient features of the numerical scheme of the software are described below details of which are available in references (13,14) .…”
Section: The Methodologymentioning
confidence: 99%