2012
DOI: 10.1016/j.paerosci.2011.10.001
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Assessment of CFD capability for prediction of hypersonic shock interactions

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Cited by 121 publications
(59 citation statements)
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References 29 publications
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“…Another comprehensive effort, again with teams working under the umbrella of AFOSR and RTO/AVT programs, culminated in a series of simulations, with high-temperature effects, which are summarized in a review article by Knight et al [118]. Fig.…”
Section: Heat Transfer and Skin Friction Coefficientmentioning
confidence: 99%
“…Another comprehensive effort, again with teams working under the umbrella of AFOSR and RTO/AVT programs, culminated in a series of simulations, with high-temperature effects, which are summarized in a review article by Knight et al [118]. Fig.…”
Section: Heat Transfer and Skin Friction Coefficientmentioning
confidence: 99%
“…In our numerical model, both the electromagnetic and flow field equations are discretized by means of a second-order accurate finite volume method implemented within COOLFluiD, [43][44][45][46][47] an open computational platform for multi-physics and plasma 30, 48-50 in particular. The COOLFluiD ICP solver relies upon the AUSM+up scheme 51 for discretizing convective fluxes and upon a central treatment of diffusive fluxes.…”
Section: Methodsmentioning
confidence: 99%
“…The latter is an open-source platform for high-performance scientific computing 3 featuring advanced computational models/ solvers for tackling re-entry aerothermodynamics (Degrez et al 2009;Lani et al 2013a;Munafo et al 2013;Garicano Mena et al 2015), simulation of experiments in highenthalpy facilities (Knight et al 2012;Zhang et al 2016), ideal magnetohydrodynamics for space weather prediction (Yalim et al 2011;Lani et al 2014), radiation transport by means of ray tracingand Monte Carlo (Santos & Lani 2016) algorithms, etc.…”
Section: Numerical Schemes and Boundary Conditionsmentioning
confidence: 99%