Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/54090
Full metadata record
DC FieldValueLanguage
dc.contributor.authorTruong, Ngoc Quoc Thang.
dc.date.accessioned2013-06-13T07:42:51Z
dc.date.available2013-06-13T07:42:51Z
dc.date.copyright2013en_US
dc.date.issued2013
dc.identifier.urihttp://hdl.handle.net/10356/54090
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.language.isoenen_US
dc.rightsNanyang Technological University
dc.subjectDRNTU::Engineeringen_US
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
item.fulltextWith Fulltext-
item.grantfulltextrestricted-
Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)
Files in This Item:
File Description SizeFormat 
FINAL REPORT.pdf
  Restricted Access
3.21 MBAdobe PDFView/Open

Page view(s)

227
Updated on Apr 15, 2021

Download(s) 50

19
Updated on Apr 15, 2021

Google ScholarTM

Check

Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.