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|Title:||Adaptive wing and fuselage structure for UAVs||Authors:||Truong, Ngoc Quoc Thang.||Keywords:||DRNTU::Engineering||Issue Date:||2013||Abstract:||In 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.||URI:||http://hdl.handle.net/10356/54090||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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