Development of a multi-rotor VTOL UAV : numerical study of the tilting-transition phase

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.

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Bibliographic Details
Main Author: Muhammmad Nur Hisyam Hussain
Other Authors: Chan Wai Lee
Format: Final Year Project
Language:English
Published: 2018
Subjects:
Online Access:http://hdl.handle.net/10356/75224
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Institution: Nanyang Technological University
Language: English