Numerical Analysis on the Effects of Blade Loading on Vortex Shedding and Boundary Layer Behavior in a Transonic Axial Compressor

Numerical Analysis on the Effects of Blade Loading on Vortex Shedding and Boundary Layer Behavior in a Transonic Axial Compressor

Multiple high-fidelity, time-accurate computational fluid dynamics simulations were performed to investigate the effects of upstream stator loading and rotor shock strength on vortex shedding characteristics in a single stage transonic compressor. Various configurations of a transonic axial compress...

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Bibliographic Details
Main Author: Clark, Kenneth Phillip
Format: Others
Published: BYU ScholarsArchive 2011
Subjects:
Kenneth Clark
turbomachinery
gas turbine engines
transonic compressor
blade row interactions
vortex shedding
stator loading
suction side boundary layer
circulation
Mechanical Engineering
Online Access:https://scholarsarchive.byu.edu/etd/2652
https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3651&context=etd

Internet

https://scholarsarchive.byu.edu/etd/2652
https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3651&context=etd

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