Performance characteristics in transonic axial compressor rotor blade using circular jets

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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
Language:	English
Published:	2016
Subjects:	Aerodynamics, Transonic Compressors - Blades
Online Access:	http://psasir.upm.edu.my/id/eprint/70648/ http://psasir.upm.edu.my/id/eprint/70648/1/FK%202016%20151%20-%20IR.pdf

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