Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/77495
Title: Flying disc-wing : development of a spinning mechanism
Authors: Ng, Eugene Jia Qi
Keywords: DRNTU::Engineering::Aeronautical engineering
Issue Date: 2019
Abstract: This paper attempts to explore the feasibility of using a flying disc-wing as an Unmanned Aerial Vehicle (UAV) by studying methods to maintain its spinning motion. A two-dimensional model of a disc-wing is built to explore the method of using propulsive forces as the main driving force. Besides using propulsive forces, an electric motor method is also studied for comparison against the propulsive method. Lastly, to further understand the concept of controlling the spinning motion, the underlying flight dynamic properties of gyroscopic precession has to be studied. This is done through a partnership with another student, Mr Tan Jun Kiat, whom focuses on the experimental portion of the project while the Computational Fluid Dynamics study is presented in this paper. A three-dimensional model of a disc-wing is built in an attempt to capture the gyroscopic precession using a quasi-steady case. This simulation will facilitate to deepen the understanding the gyroscopic precession of a flying disc-wing UAV.
URI: http://hdl.handle.net/10356/77495
Schools: School of Mechanical and Aerospace Engineering 
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:
File Description SizeFormat 
B288_NG_JQE_20190506.pdf
  Restricted Access
Main Report1.74 MBAdobe PDFView/Open

Page view(s)

237
Updated on Jun 19, 2024

Download(s)

10
Updated on Jun 19, 2024

Google ScholarTM

Check

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