Study of aerodynamics on the analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computatonal Fluid Dynamics (CFD) for high subsonic flow / Mohd Yusof Safaruddin Abdulawi

This thesis presents a study of Aerodynamic of a Blended Wing Body Unmanned Aircraft Vehicle (BWB UAV) within a UiTM project. A computational analysis is being carried out throughout the process through Computational Fluid Dynamics (CFD) software (FLUENT) which computed the steady, three-dimensional...

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Main Author:	Abdulawi, Mohd Yusof Safaruddin
Format:	Thesis
Language:	English
Published:	2006
Subjects:	Aeronautics Aeronautical engineering
Online Access:	https://ir.uitm.edu.my/id/eprint/37224/1/37224.pdf
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id	my-uitm-ir.37224
record_format	uketd_dc
spelling	my-uitm-ir.372242020-11-20T01:50:29Z Study of aerodynamics on the analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computatonal Fluid Dynamics (CFD) for high subsonic flow / Mohd Yusof Safaruddin Abdulawi 2006 Abdulawi, Mohd Yusof Safaruddin Aeronautics. Aeronautical engineering This thesis presents a study of Aerodynamic of a Blended Wing Body Unmanned Aircraft Vehicle (BWB UAV) within a UiTM project. A computational analysis is being carried out throughout the process through Computational Fluid Dynamics (CFD) software (FLUENT) which computed the steady, three-dimensional using the standard one-equation Spalart-Allmaras turbulence model. A comparison of meshing is being completed between the unrefined, refined, and adapted mesh sizes. The three-dimensional BWB Aerodynamic characteristics are validated using two-dimensional transonic airfoil at various angles of attack. This thesis starts with literature overview then followed with mathematical model used in the analysis. Overview of Aerodynamics terminologies is presented in Chapter 3 and proceeds with the CFD general theory in the next chapter. Chapter 6 and 7 presents extensive discussions of numerical simulation and the outcome of simulation respectively throughout this project. This thesis is ended with conclusion and recommendation at the end of the chapter. 2006 Thesis https://ir.uitm.edu.my/id/eprint/37224/ https://ir.uitm.edu.my/id/eprint/37224/1/37224.pdf text en public degree Universiti Teknologi MARA Faculty of Mechanical Engineering Effendy, Rizal
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Effendy, Rizal
topic	Aeronautics Aeronautical engineering
spellingShingle	Aeronautics Aeronautical engineering Abdulawi, Mohd Yusof Safaruddin Study of aerodynamics on the analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computatonal Fluid Dynamics (CFD) for high subsonic flow / Mohd Yusof Safaruddin Abdulawi
description	This thesis presents a study of Aerodynamic of a Blended Wing Body Unmanned Aircraft Vehicle (BWB UAV) within a UiTM project. A computational analysis is being carried out throughout the process through Computational Fluid Dynamics (CFD) software (FLUENT) which computed the steady, three-dimensional using the standard one-equation Spalart-Allmaras turbulence model. A comparison of meshing is being completed between the unrefined, refined, and adapted mesh sizes. The three-dimensional BWB Aerodynamic characteristics are validated using two-dimensional transonic airfoil at various angles of attack. This thesis starts with literature overview then followed with mathematical model used in the analysis. Overview of Aerodynamics terminologies is presented in Chapter 3 and proceeds with the CFD general theory in the next chapter. Chapter 6 and 7 presents extensive discussions of numerical simulation and the outcome of simulation respectively throughout this project. This thesis is ended with conclusion and recommendation at the end of the chapter.
format	Thesis
qualification_level	Bachelor degree
author	Abdulawi, Mohd Yusof Safaruddin
author_facet	Abdulawi, Mohd Yusof Safaruddin
author_sort	Abdulawi, Mohd Yusof Safaruddin
title	Study of aerodynamics on the analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computatonal Fluid Dynamics (CFD) for high subsonic flow / Mohd Yusof Safaruddin Abdulawi
title_short	Study of aerodynamics on the analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computatonal Fluid Dynamics (CFD) for high subsonic flow / Mohd Yusof Safaruddin Abdulawi
title_full	Study of aerodynamics on the analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computatonal Fluid Dynamics (CFD) for high subsonic flow / Mohd Yusof Safaruddin Abdulawi
title_fullStr	Study of aerodynamics on the analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computatonal Fluid Dynamics (CFD) for high subsonic flow / Mohd Yusof Safaruddin Abdulawi
title_full_unstemmed	Study of aerodynamics on the analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computatonal Fluid Dynamics (CFD) for high subsonic flow / Mohd Yusof Safaruddin Abdulawi
title_sort	study of aerodynamics on the analysis for blended wing body (bwb) unmanned aerial vehicle (uav) using computatonal fluid dynamics (cfd) for high subsonic flow / mohd yusof safaruddin abdulawi
granting_institution	Universiti Teknologi MARA
granting_department	Faculty of Mechanical Engineering
publishDate	2006
url	https://ir.uitm.edu.my/id/eprint/37224/1/37224.pdf
_version_	1783734405342167040

Study of aerodynamics on the analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computatonal Fluid Dynamics (CFD) for high subsonic flow / Mohd Yusof Safaruddin Abdulawi

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