Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/54090
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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