Development of a multi-rotor VTOL UAV : computation of aerodynamics forces and moments using CFD

A VTOL model aircraft is analysed using CFD code. The model was first conceptually designed using a simplified design code XFLR5, and a full detailed assessment of the model is performed. Detailed mesh independence studies were performed and the results for longitudinal motion were obtained. Furt...

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Bibliographic Details
Main Author: Tan, Dion Jin Yan
Other Authors: Basman Elhadidi
Format: Final Year Project
Language:English
Published: 2018
Subjects:
Online Access:http://hdl.handle.net/10356/75581
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Institution: Nanyang Technological University
Language: English