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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Format: | Others |
Language: | English |
Published: |
2012
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Online Access: | http://hdl.handle.net/2152/ETD-UT-2012-05-5155 |