Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam

This thesis represents the study on aerodynamics of a Blended Wing Body Unmanned Aircraft Ve-hicle (BWB UAV) at a low subsonic speed for elevator deflection of - 15°. Elevator is one of im-portant parts in aircraft desigbn where it can acts as a control surface that influencing the nose up and down...

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Main Author:	Jundam, Mohd. Fazil
Format:	Thesis
Language:	English
Published:	2009
Subjects:	Mechanics of engineering Applied mechanics
Online Access:	https://ir.uitm.edu.my/id/eprint/31242/1/31242.PDF
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id	my-uitm-ir.31242
record_format	uketd_dc
spelling	my-uitm-ir.312422022-06-08T07:48:07Z Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam 2009 Jundam, Mohd. Fazil Mechanics of engineering. Applied mechanics This thesis represents the study on aerodynamics of a Blended Wing Body Unmanned Aircraft Ve-hicle (BWB UAV) at a low subsonic speed for elevator deflection of - 15°. Elevator is one of im-portant parts in aircraft desigbn where it can acts as a control surface that influencing the nose up and down during pitching motion of the aircraft. This project started with the construction of the BWB model and deflecting the elevator section into - 15° (Upward) by using CATIA V5 R16. 2009 Thesis https://ir.uitm.edu.my/id/eprint/31242/ https://ir.uitm.edu.my/id/eprint/31242/1/31242.PDF text en public degree Universiti Teknologi MARA Shah Alam Faculty of Mechanical Engineering, Universiti Teknologi MARA Shah Alam Wisnoe, Wirachman (Ass. Prof. Dr.)
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Wisnoe, Wirachman (Ass. Prof. Dr.)
topic	Mechanics of engineering Applied mechanics
spellingShingle	Mechanics of engineering Applied mechanics Jundam, Mohd. Fazil Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam
description	This thesis represents the study on aerodynamics of a Blended Wing Body Unmanned Aircraft Ve-hicle (BWB UAV) at a low subsonic speed for elevator deflection of - 15°. Elevator is one of im-portant parts in aircraft desigbn where it can acts as a control surface that influencing the nose up and down during pitching motion of the aircraft. This project started with the construction of the BWB model and deflecting the elevator section into - 15° (Upward) by using CATIA V5 R16.
format	Thesis
qualification_level	Bachelor degree
author	Jundam, Mohd. Fazil
author_facet	Jundam, Mohd. Fazil
author_sort	Jundam, Mohd. Fazil
title	Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam
title_short	Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam
title_full	Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam
title_fullStr	Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam
title_full_unstemmed	Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam
title_sort	computational fluid dynamics (cfd) analysis of a blended wing body (bwb) unmanned aerial vehicle (uav) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / mohd. fazil jundam
granting_institution	Universiti Teknologi MARA Shah Alam
granting_department	Faculty of Mechanical Engineering, Universiti Teknologi MARA Shah Alam
publishDate	2009
url	https://ir.uitm.edu.my/id/eprint/31242/1/31242.PDF
_version_	1783734108902391808

Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam

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