Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/75725
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dc.contributor.authorTang, Weiyi-
dc.date.accessioned2018-06-11T08:18:33Z-
dc.date.available2018-06-11T08:18:33Z-
dc.date.issued2018-
dc.identifier.urihttp://hdl.handle.net/10356/75725-
dc.description.abstractFlapping wing micro air vehicle (FWMAV), different from fixed-wing and rotary wing aircraft, remains experimental in its application. However, its study has much potential because of its extraordinary agility, structural simplicity and aerodynamic efficiency. The author was inspired to test the effect of combining two sets of flapping wings, with focus on developing a pitching control by altering the speed differential of the two flapping-wing sections. This is actualized by offsetting thrust vector with center of gravity.en_US
dc.format.extent51 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University-
dc.subjectDRNTU::Engineering::Aeronautical engineering::Aircraften_US
dc.titleDragonfly-like air vehicleen_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorLau Gih Keongen_US
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.description.degreeBachelor of Engineering (Aerospace Engineering)en_US
item.grantfulltextrestricted-
item.fulltextWith Fulltext-
Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)
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