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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.copyright2018
dc.date.issued2018
dc.identifier.otherID 14321011
dc.identifier.otherID 13321083
dc.identifier.otherID 14321054
dc.identifier.otherID 14110011
dc.identifier.urihttp://hdl.handle.net/10361/10052
dc.descriptionThis thesis is submitted in partial fulfilment of the requirements for the degree of Bachelor of Science in Electrical and Electronic Engineering, 2018.en_US
dc.descriptionCatalogued from PDF version of thesis.
dc.descriptionIncludes bibliographical references (page 114-118).
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.en_US
dc.description.statementofresponsibilityMohammad Mohtasim Hamid Pial
dc.description.statementofresponsibilityRidwan Bayezid
dc.description.statementofresponsibilityMd.Rezaul Karim
dc.description.statementofresponsibilityReazad Islam
dc.format.extent118 pages
dc.language.isoenen_US
dc.publisherBRAC Univeristyen_US
dc.rightsBRAC University theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission.
dc.subjectElectric aircraften_US
dc.titleElectric aircraft with HTS (High Temperature Superconductor) motor, eesign & simulationen_US
dc.typeThesisen_US
dc.contributor.departmentDepartment of Electrical and Electronic Engineering, BRAC University
dc.description.degreeB. Electrical and Electronic Engineering


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