Please use this identifier to cite or link to this item:
|Title:||Development of a multi-rotor VTOL UAV : numerical study of the tilting-transition phase||Authors:||Muhammmad Nur Hisyam Hussain||Keywords:||DRNTU::Engineering
|Issue Date:||2018||Abstract:||Development of Numerical Simulation Capability through CFD to analyse aerodynamic effects on UAV body during transition for a 2D case. Analyses of the acceptable tilt rates appropriate for level transitions for a 2D case.||URI:||http://hdl.handle.net/10356/75224||Rights:||Nanyang Technological University||Fulltext Permission:||restricted||Fulltext Availability:||With Fulltext|
|Appears in Collections:||MAE Student Reports (FYP/IA/PA/PI)|
Files in This Item:
|FYP Report [B368] - Muhammad Nur Hisyam Bin Hussain (U1420053F).pdf|
|3.13 MB||Adobe PDF||View/Open|
Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.