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REDUCED ORDER MODELING OF FLOW OVER A NACA 0015 AIRFOIL FOR FUTURE CONTROL APPLICATION

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Identiferoai:union.ndltd.org:OhioLink/oai:etd.ohiolink.edu:miami1407295741
Date11 August 2014
CreatorsSullivan, Taylor D.
PublisherMiami University / OhioLINK
Source SetsOhiolink ETDs
LanguageEnglish
Detected LanguageEnglish
Typetext
Sourcehttp://rave.ohiolink.edu/etdc/view?acc_num=miami1407295741
Rightsunrestricted, This thesis or dissertation is protected by copyright: all rights reserved. It may not be copied or redistributed beyond the terms of applicable copyright laws.

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