A study of roughness in turbulent hypersonic boundary-layers
The influence of large scale regular roughness on a Mach 5 turbulent boundary layer and a compression corner was investigated on axisymmetric wind tunnel models. Three types of roughness were examined; a series of square cavities at two different sizes and a 45 degree sawtooth. Typical sizes ranged...
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| Language: | en |
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Cranfield University
2012
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/7586 |
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