Development of a hybrid DSMC/CFD method for hypersonic boundary layer flow over discrete surface roughness

This work is focused on the development of a hybrid DSMC/CFD solver to examine hypersonic boundary layer flow over discrete surface roughness. The purpose of these investigations is to identify and quantify the non-equilibrium effects that influence the roughness-induced disturbance field and surfa...

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Bibliographic Details
Main Author: Stephani, Kelly Ann
Format: Others
Language:English
Published: 2012
Subjects:
CFD
Online Access:http://hdl.handle.net/2152/ETD-UT-2012-05-5155