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Title: Dragonfly-like air vehicle
Authors: Tang, Weiyi
Keywords: DRNTU::Engineering::Aeronautical engineering::Aircraft
Issue Date: 2018
Abstract: Flapping 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.
Schools: School of Mechanical and Aerospace Engineering 
Rights: Nanyang Technological University
Fulltext Permission: restricted
Fulltext Availability: With Fulltext
Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)

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