Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris

This thesis presents a study of Aerodynamic of a Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection using wind tunnel test. This project is the continuation of previous research using low speed wind tunnel test and the Computational Fluids Dynamics (CFD) simulation. The s...

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التفاصيل البيبلوغرافية
المؤلف الرئيسي:	Che Wan Idris, Che Wan Zaidie
التنسيق:	أطروحة
اللغة:	English
منشور في:	2009
الموضوعات:	Aeronautics Aeronautical engineering
الوصول للمادة أونلاين:	https://ir.uitm.edu.my/id/eprint/30866/1/30866.pdf
الوسوم:	إضافة وسم لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!

id	my-uitm-ir.30866
record_format	uketd_dc
spelling	my-uitm-ir.308662020-06-03T07:54:04Z Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris 2009 Che Wan Idris, Che Wan Zaidie Aeronautics. Aeronautical engineering This thesis presents a study of Aerodynamic of a Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection using wind tunnel test. This project is the continuation of previous research using low speed wind tunnel test and the Computational Fluids Dynamics (CFD) simulation. The study will focus on the aerodynamic characteristics at various angles of attack at 0.1 - 0.15 Mach number using wind tunnel test at Low Subsonic speed. The purpose of this project is to measure the aerodynamic characteristics such as lift coefficient, drag coefficient and pitching moment coefficient of BWB UAV using the wind tunnel test with modified elevator angle at -5 and +5 deflection 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/30866/ https://ir.uitm.edu.my/id/eprint/30866/1/30866.pdf text en public degree Universiti Teknologi MARA Faculty of Mechanical Engineering Wisnoe, Wirachman (Dr)
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Wisnoe, Wirachman (Dr)
topic	Aeronautics Aeronautical engineering
spellingShingle	Aeronautics Aeronautical engineering Che Wan Idris, Che Wan Zaidie Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris
description	This thesis presents a study of Aerodynamic of a Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection using wind tunnel test. This project is the continuation of previous research using low speed wind tunnel test and the Computational Fluids Dynamics (CFD) simulation. The study will focus on the aerodynamic characteristics at various angles of attack at 0.1 - 0.15 Mach number using wind tunnel test at Low Subsonic speed. The purpose of this project is to measure the aerodynamic characteristics such as lift coefficient, drag coefficient and pitching moment coefficient of BWB UAV using the wind tunnel test with modified elevator angle at -5 and +5 deflection 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	Che Wan Idris, Che Wan Zaidie
author_facet	Che Wan Idris, Che Wan Zaidie
author_sort	Che Wan Idris, Che Wan Zaidie
title	Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris
title_short	Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris
title_full	Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris
title_fullStr	Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris
title_full_unstemmed	Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris
title_sort	experimental aerodynamics of blended wing body (bwb) unmanned aerial vehicle (uav) with elevator deflection of +5° and -5° using wind tunnel (mach number 0.1-0.15) / che wan zaidie che wan idris
granting_institution	Universiti Teknologi MARA
granting_department	Faculty of Mechanical Engineering
publishDate	2009
url	https://ir.uitm.edu.my/id/eprint/30866/1/30866.pdf
_version_	1783734090983276544

Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris

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