Development of a boundary layer control device for tip clearence experiments in an axial compressor
A boundary layer control device was designed to change significantly the case-wall boundary layer thickness entering a large-scale, multistage axial compressor. The device was intended to double the boundary layer thickness in order to evaluate the influence of the inlet boundary layer in controlled...
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| Language: | en_US |
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Monterey, California : Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/23016 |