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Parametric study of hypersonic boundary layer flow over discrete surface roughness using a Hybrid DSMC/Navier-Stokes Solver

Stephani, K., Goldstein, D., and Varghese, P., “Parametric Study of Hypersonic Boundary Layer Flow over Discrete Surface Roughness Using a Hybrid DSMC/Navier- Stokes Solver’’ AIAA paper 2011-3250 presented at the AIAA Fluid Dynamics Mtg. Honolulu, June 2011.