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dc.contributor.advisorJanus, J. Mark
dc.contributor.authorRighi, Hajar
dc.date2016
dc.date.accessioned2020-08-14T15:55:44Z
dc.date.available2020-08-14T15:55:44Z
dc.identifier.urihttps://hdl.handle.net/11668/18619
dc.description.abstractThe main concerns of air travel are the operating costs of general aviation aircraft. Hybrid-electric system design provides a great opportunity for future aircraft models to be environmentally friendly. The Hybrid-electric power propulsion system experienced a growing interest driven by determined targets. Electric technologies have proven promising success to achieve a successful result in the near- and long-term. Combining fuel cells and batteries, this technology can enable a significant reduction in fuel consumption, noise, and emissions. Different types of fuel cells and batteries are proposed and discussed during this work. The Cessna C-172 is a candidate to test the combination of the most promising fuel cells and batteries for a hybridization or complete electrification strategy.
dc.publisherMississippi State University
dc.subject.otherSolide Oxide fuel cell and Lithium Sulfur battery
dc.titleHybrid Electric Aircraft
dc.typeThesis
dc.publisher.departmentDepartment of Aerospace Engineering
dc.publisher.collegeBagley College of Engineering
dc.date.authorbirth1993
dc.subject.degreeMaster of Science
dc.subject.majorAerospace Engineering
dc.contributor.committeeOlsen, Gregory
dc.contributor.committeeBelk, Davy M.


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