The fidelity of DSMC method to analyze the aerothermodynamics of the pure continuum flow regime

Performance Analyses of Fluidic Thrust Vector Control System Using Dual Throat Nozzle

“…Close agreement existed between the hybrid simulations' results and the experimental data at various Mach numbers' cases. Recently, Hasan [11] reported that the pure DSMC method was used to compute hypersonic flow around an aeroshell during atmospheric reentry. The flowfield contains both continuum and rarefied regions.…”