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Control of Hypersonic High Angle-Of-Attack Re-Entry Flow Using a Semi-Empirical Plasma Actuator Model

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Identiferoai:union.ndltd.org:OhioLink/oai:etd.ohiolink.edu:dayton1335283726
Date11 May 2012
CreatorsAtkinson, Michael D.
PublisherUniversity of Dayton / OhioLINK
Source SetsOhiolink ETDs
LanguageEnglish
Detected LanguageEnglish
Typetext
Sourcehttp://rave.ohiolink.edu/etdc/view?acc_num=dayton1335283726
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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