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....

Full description

Saved in:
Bibliographic Details
Main Author: Epsipha, Pauline
Format: Thesis
Language:English
Published: 2016
Subjects:
Online Access:http://psasir.upm.edu.my/id/eprint/70648/1/FK%202016%20151%20-%20IR.pdf
Tags: Add Tag
No Tags, Be the first to tag this record!

Similar Items