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dc.contributor.authorTruong, Ngoc Quoc Thang.
dc.description.abstractIn recent years, inflated structure is being widely applied for adaptive UAVs due to its exceptional characteristics, including weight-saving, survivability after collision and easily configured. These wonderful characteristics enable the UAVs to be contractible/deployable, warping and morphing wing. However, there are still serious short-comings with these inflated wings, including the ultra-high compressed-air pressure, difficulty in wing-profile shaping and unreliable. Hence this project proposes a new design that uses Planar Kagome lattice to reinforce the core air-beam.en_US
dc.format.extent67 p.en_US
dc.rightsNanyang Technological University
dc.titleAdaptive wing and fuselage structure for UAVsen_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorK Radhakrishnanen_US
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.description.degreeBachelor of Engineering (Aerospace Engineering)en_US
dc.contributor.supervisor2Seung Ki Moonen_US
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Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)
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