2014
DOI: 10.1016/j.ast.2014.07.005
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Heat reduction using conterflowing jet for a nose cone with aerodisk in hypersonic flow

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Cited by 105 publications
(20 citation statements)
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“…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%
“…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%
“…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%
“…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%