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A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor

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1. http://rave.ohiolink.edu/etdc/view?acc_num=ucin150479438822623

Identifer	oai:union.ndltd.org:OhioLink/oai:etd.ohiolink.edu:ucin150479438822623
Date	07 November 2017
Creators	Heberling, Brian
Publisher	University of Cincinnati / OhioLINK
Source Sets	Ohiolink ETDs
Language	English
Detected Language	English
Type	text
Source	http://rave.ohiolink.edu/etdc/view?acc_num=ucin150479438822623
Rights	unrestricted, This thesis or dissertation is protected by copyright: some rights reserved. It is licensed for use under a Creative Commons license. Specific terms and permissions are available from this document's record in the OhioLINK ETD Center.