A modular particle-continuum numerical method for hypersonic non-equilibrium gas flows

Journal of Computational Physics

Volumn 225, Issue 1, 2007, Pages 1159-1174

  Schwartzentruber, T E ^a   Scalabrin, L C ^a   Boyd, I D ^a  

^a University of Michigan   (United States)

Author keywords

Direct simulation Monte Carlo; DSMC; Hybrid particle continuum; Hypersonics; Non equilibrium flow; Rarefied flow; Re entry vehicles

Indexed keywords

HYPERSONIC FLOW; HYPERSONIC VEHICLES; MONTE CARLO METHODS; NAVIER STOKES EQUATIONS; NUMERICAL METHODS; VELOCITY CONTROL;

DIRECT SIMULATION MONTE CARLO; HYBRID FUNCTIONS; HYBRID PARTICLE-CONTINUUM; HYBRID PARTICLES; MODULARS; NON EQUILIBRIUM; NON-EQUILIBRIUM FLOWS; RAREFIED FLOW; RE-ENTRY VEHICLES;

FLOW OF GASES;

EID: 34447251045     PISSN: 00219991     EISSN: 10902716     Source Type: Journal    
DOI: 10.1016/j.jcp.2007.01.022     Document Type: Article

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