AXIAL COMPRESSOR FLOW BEHAVIOR NEAR THE AERODYNAMIC STABILITY LIMIT

AXIAL COMPRESSOR FLOW BEHAVIOR NEAR THE AERODYNAMIC STABILITY LIMIT

In this investigation, casing mounted high frequency response pressure transducers are used to characterize the flow behavior near the aerodynamic stability limit of a low speed single stage axial flow compressor. Time variant pressure measurements are acquired at discrete operating points up to the...

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Bibliographic Details
Main Author: Butler, Bradley D.
Format: Others
Published: UKnowledge 2014
Subjects:
Turbomachines
Axial Compressor
Stall Inception
Modal Stall
Compressor Stability
Energy Systems
Online Access:http://uknowledge.uky.edu/me_etds/34
http://uknowledge.uky.edu/cgi/viewcontent.cgi?article=1037&context=me_etds

Internet

http://uknowledge.uky.edu/me_etds/34
http://uknowledge.uky.edu/cgi/viewcontent.cgi?article=1037&context=me_etds

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