Electric aircraft with HTS (High Temperature Superconductor) motor, eesign & simulation

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dc.contributor.advisorAzad, Dr. AKM Abdul Malek
dc.contributor.authorPial, Mohammad Mohtasim Hamid
dc.contributor.authorBayezid, Ridwan
dc.contributor.authorKarim, Md.Rezaul
dc.contributor.authorIslam, Reazad
dc.date.accessioned2018-05-08T09:53:15Z
dc.date.available2018-05-08T09:53:15Z
dc.date.issued2018
dc.descriptionCatalogued from PDF version of thesis.
dc.descriptionIncludes bibliographical references (page 114-118).
dc.descriptionThis thesis is submitted in partial fulfilment of the requirements for the degree of Bachelor of Science in Electrical and Electronic Engineering, 2018.
dc.description.abstractEvolution of electric aircrafts would allow more efficient, quiet and green transports that would reduce the emission of greenhouse gases along with reduction in the overall flight expenses, which conventional IC engines are incapable of. This thesis concerns the possibility of designing an efficient electrical aircraft by considering AURORA D8 body structure. The AURORA D8 or the double bubble design is currently under development by NASA and is predicted to hit the market by 2035. The aircraft will be powered by HTS motor, the armature coil of which will be made of YBCO. The simulation of the motor is carried out by FEA software COMSOL 5.3. A cryocooler is designed and its simulation is done in ANSYS.
dc.identifier.otherID 14321011
dc.identifier.otherID 13321083
dc.identifier.otherID 14321054
dc.identifier.otherID 14110011
dc.identifier.otherhttps://dspace.bracu.ac.bd/server/api/core/items/fc1ac42a-f10b-4088-9277-ad6e6b7e6869
dc.identifier.urihttp://hdl.handle.net/10361/10052
dc.language.isoen
dc.publisherBRAC University
dc.sourceBRAC University Institutional Repository
dc.subjectElectric aircraft
dc.titleElectric aircraft with HTS (High Temperature Superconductor) motor, eesign & simulation
dc.typeThesis

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Thesis & Design Report (Bachelor of Science in Electrical and Electronic Engineering)