A cell-based coupling of DSMC and MD with lifting and restricting operators is demonstrated, reducing surface temperature prediction error in a hypersonic flow from 730% to 4.4% relative to experiment.
Votta,Hypersonic high altitude aerothermodynamics of a space re-entry vehicle, Aerospace Science and Technology, 2013
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A Concurrent Multiscale Framework Coupling Direct Simulation Monte Carlo and Molecular Dynamics
A cell-based coupling of DSMC and MD with lifting and restricting operators is demonstrated, reducing surface temperature prediction error in a hypersonic flow from 730% to 4.4% relative to experiment.