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dc.contributor.advisorPapadakis, Michael
dc.contributor.authorBikkannavar, Karan Vishwanath
dc.date.accessioned2016-11-14T21:53:49Z
dc.date.available2016-11-14T21:53:49Z
dc.date.issued2016-05
dc.identifier.othert16002
dc.identifier.urihttp://hdl.handle.net/10057/12647
dc.descriptionThesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering
dc.description.abstractThe new trend in aviation industry is towards „all electric aircraft‟. Thus, there‟s a strong desire to replace bleed air systems with efficient electrical ice protection systems that would provide adequate ice protection. In the current thesis study, a computational methodology was developed to support the design and assess the performance of electro-thermal ice protection systems (ETIPS) for de-icing fixed wing aircraft. The methodology developed was tested using a range of geometries and electrical heater configurations and was validated with experimental data obtained by researchers at Wichita State University (WSU) and other organizations.
dc.format.extentxiv, 98 p.
dc.language.isoen_US
dc.publisherWichita State University
dc.rightsCopyright 2016 Karan Vishwanath Bikkannavar
dc.subject.lcshElectronic dissertations
dc.titleComputational methodology for electro-thermal ice protection system analysis
dc.typeThesis


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  • AE Theses and Dissertations [137]
    Electronic copies of theses and dissertations defended in the Department of Aerospace Engineering
  • Master's Theses [1383]
    This collection includes Master's theses completed at the Wichita State University Graduate School (Fall 2005 --)

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