Development of a multi-rotor VTOL UAV : numerical study of the tilting-transition phase
Muhammmad Nur Hisyam Hussain
Date of Issue2018
School of Mechanical and Aerospace Engineering
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.
Final Year Project (FYP)
Nanyang Technological University