2011
DOI: 10.1260/1759-3107.2.1.1
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Numerical Study on Heat Reduction of Various Counterflowing Jets over Highly Blunt Cone in Hypersonic Flow

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Cited by 23 publications
(4 citation statements)
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“…The simulations were performed using an implicit CFD code [35][36][37][38][39][40][41][42]. In this code, the cell centered finite volume approach is used to solve three-dimensional Reynolds-average Navier-Stokes (RANS) equations.…”
Section: Numerical Proceduresmentioning
confidence: 99%
See 1 more Smart Citation
“…The simulations were performed using an implicit CFD code [35][36][37][38][39][40][41][42]. In this code, the cell centered finite volume approach is used to solve three-dimensional Reynolds-average Navier-Stokes (RANS) equations.…”
Section: Numerical Proceduresmentioning
confidence: 99%
“…A second order upwind scheme was used to discretize both momentum, continuity and energy equations with a coupled solver. The convective fluxes were treated using the Roe Flux-Difference Splitting Scheme, which has been shown to enhance the accuracy of shocks [37]. The fuel jet is hydrogen, with the pressure, temperature and density being coupled using the ideal gas law.…”
Section: Numerical Proceduresmentioning
confidence: 99%
“…The simulations were performed using an implicit CFD code [33][34][35][36][37][38][39]. This code solves NavierStokes equations using cell centered finite volume approach.…”
Section: Treatment Of Numericalmentioning
confidence: 99%
“…We should remark that in general conditions where asymmetry is also allowed, infinitely many solutions exist [38][39][40][41][42][43][44][45][46]. To keep the symmetry with regard to the centerline, we visit the same stretching/shrinking rates on both walls.…”
Section: Problem Definitionmentioning
confidence: 99%