Performance characteristics in transonic axial compressor rotor blade using circular jets

The reduction of the flow separation region or even eliminating it from the transonic axial flow compressor has been a motivating research area as it reduces turbulence and modifies the flow field into more desired state. Even a small performance improvement could be a big help in saving fuel cost....

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Bibliographic Details
Main Author: Epsipha, Pauline
Format: Thesis
Published: 2016
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