End-wall flows and blading design for axial flow compressors
The flow in multistage axial flow compressors is particularly complex in nature because of the proximity of moving bladerows, the growth of end-wall boundary layers and the presence of tip and seal leakages and secondary flow. The problems associated with these phenomena are at their most acute in t...
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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/1826/6929 |
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