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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Cranfield University
1993
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| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.358329 |