Transition to turbulence in a turbomachinery environment
This thesis aims to contribute to the understanding of transitional flows in the blade boundary layers of axial compressors. Two experiments are described, the first examining in detail the transitional boundary layer on a simulated controlled-diffusion blade and the second surveying the mid-height...
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| Language: | en |
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Cranfield University
2016
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/10509 |