Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali

This thesis presents a study of aerodynamic of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel. This project is the continuation of previous research using Low Speed Tunnel LST and Computational Fluids Dynamics (CFD) simulation and is...

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Bibliographic Details
Main Author:	Wan Razali, Wan Mohd Hafizan
Format:	Thesis
Language:	English
Published:	2009
Subjects:	Machinery exclusive of prime movers Machine design and drawing
Online Access:	https://ir.uitm.edu.my/id/eprint/36061/1/36061.pdf
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id	my-uitm-ir.36061
record_format	uketd_dc
spelling	my-uitm-ir.360612020-11-04T05:02:16Z Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali 2009 Wan Razali, Wan Mohd Hafizan Machinery exclusive of prime movers Machine design and drawing This thesis presents a study of aerodynamic of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel. This project is the continuation of previous research using Low Speed Tunnel LST and Computational Fluids Dynamics (CFD) simulation and is very important to validate the result it. This project will present the Analysis of BWB Aerodynamics at low subsonic speed. The study will focus on the aerodynamic characteristics at various angles of attack at 0.1 Mach number using wind tunnel test. The objective of this project is to obtain the aerodynamic characteristics such as lift coefficient, drag coefficient and pitching moment coefficient of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel and also to observe the quality of flow pattern around the BWB UAV at various angles of attack using flow visualization techniques. 2009 Thesis https://ir.uitm.edu.my/id/eprint/36061/ https://ir.uitm.edu.my/id/eprint/36061/1/36061.pdf text en public degree Universiti Teknologi MARA Faculty of Mechanical Engineering Wisnoe, Wirachman (Prof. Madya Dr.)
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Wisnoe, Wirachman (Prof. Madya Dr.)
topic	Machinery exclusive of prime movers Machine design and drawing
spellingShingle	Machinery exclusive of prime movers Machine design and drawing Wan Razali, Wan Mohd Hafizan Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
description	This thesis presents a study of aerodynamic of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel. This project is the continuation of previous research using Low Speed Tunnel LST and Computational Fluids Dynamics (CFD) simulation and is very important to validate the result it. This project will present the Analysis of BWB Aerodynamics at low subsonic speed. The study will focus on the aerodynamic characteristics at various angles of attack at 0.1 Mach number using wind tunnel test. The objective of this project is to obtain the aerodynamic characteristics such as lift coefficient, drag coefficient and pitching moment coefficient of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel and also to observe the quality of flow pattern around the BWB UAV at various angles of attack using flow visualization techniques.
format	Thesis
qualification_level	Bachelor degree
author	Wan Razali, Wan Mohd Hafizan
author_facet	Wan Razali, Wan Mohd Hafizan
author_sort	Wan Razali, Wan Mohd Hafizan
title	Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
title_short	Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
title_full	Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
title_fullStr	Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
title_full_unstemmed	Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
title_sort	experimental aerodynamics of blended wing body (bwb) unmanned aerial vehicle (uav) with elevator deflection of +15° and -15° using wind tunnel (mach number 0.1-0.15) / wan mohd hafizan wan razali
granting_institution	Universiti Teknologi MARA
granting_department	Faculty of Mechanical Engineering
publishDate	2009
url	https://ir.uitm.edu.my/id/eprint/36061/1/36061.pdf
_version_	1783734322714378240

Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali

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