Computational fluid dynamic (CFD) analysis of blended wing body (BWB) Baseline-II unmanned aerial vehicle (UAV) with canard setting angle of 10° at 0.1mach number / Nik Ahmad Khalil Badiruddeen

This study investigates the effect of canard on the aerodynamic characteristics of MARA University of Technology's (UiTM) Blended Wing Body (BWB) Baseline-II of Unmanned Aerial Vehicle (UAV) aircraft design. Canard is a small lifting wing located in front of the main wing which is used to impro...

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Main Author:	Badiruddeen, Nik Ahmad Khalil
Format:	Thesis
Language:	English
Published:	2010
Subjects:	Fluid dynamics
Online Access:	https://ir.uitm.edu.my/id/eprint/67306/1/67306.pdf
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id	my-uitm-ir.67306
record_format	uketd_dc
spelling	my-uitm-ir.673062022-09-23T03:14:17Z Computational fluid dynamic (CFD) analysis of blended wing body (BWB) Baseline-II unmanned aerial vehicle (UAV) with canard setting angle of 10° at 0.1mach number / Nik Ahmad Khalil Badiruddeen 2010 Badiruddeen, Nik Ahmad Khalil Fluid dynamics This study investigates the effect of canard on the aerodynamic characteristics of MARA University of Technology's (UiTM) Blended Wing Body (BWB) Baseline-II of Unmanned Aerial Vehicle (UAV) aircraft design. Canard is a small lifting wing located in front of the main wing which is used to improve lift and provide adequate flight stability of the BWB Baseline-II. The implementations of Computational Fluids Dynamics (CFD) have accelerated the aerodynamics predictions of the BWB Baseline-II design conducted at the same conditions with actual flying BWB size at various angles of attack. Lift coefficient (CL), drag coefficient (Co) and pitching moment coefficient (CM) are studied at flight condition of 0.1 Mach number with respect to canard deflection angle of 10°. This project begins with some modification of canard deflection angle of the BWB's CAD model to 10°. The modified model is then imported into CFD software for meshing and simulation processes. The relationship between CL, CD, and CM, visualization of pressure contours, Mach number contours, and airflow, around the aircraft being investigated and analyzed. 2010 Thesis https://ir.uitm.edu.my/id/eprint/67306/ https://ir.uitm.edu.my/id/eprint/67306/1/67306.pdf text en public degree Universiti Teknologi MARA (UiTM) Faculty of Mechanical Engineering Wisnoe, Wirachman
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Wisnoe, Wirachman
topic	Fluid dynamics
spellingShingle	Fluid dynamics Badiruddeen, Nik Ahmad Khalil Computational fluid dynamic (CFD) analysis of blended wing body (BWB) Baseline-II unmanned aerial vehicle (UAV) with canard setting angle of 10° at 0.1mach number / Nik Ahmad Khalil Badiruddeen
description	This study investigates the effect of canard on the aerodynamic characteristics of MARA University of Technology's (UiTM) Blended Wing Body (BWB) Baseline-II of Unmanned Aerial Vehicle (UAV) aircraft design. Canard is a small lifting wing located in front of the main wing which is used to improve lift and provide adequate flight stability of the BWB Baseline-II. The implementations of Computational Fluids Dynamics (CFD) have accelerated the aerodynamics predictions of the BWB Baseline-II design conducted at the same conditions with actual flying BWB size at various angles of attack. Lift coefficient (CL), drag coefficient (Co) and pitching moment coefficient (CM) are studied at flight condition of 0.1 Mach number with respect to canard deflection angle of 10°. This project begins with some modification of canard deflection angle of the BWB's CAD model to 10°. The modified model is then imported into CFD software for meshing and simulation processes. The relationship between CL, CD, and CM, visualization of pressure contours, Mach number contours, and airflow, around the aircraft being investigated and analyzed.
format	Thesis
qualification_level	Bachelor degree
author	Badiruddeen, Nik Ahmad Khalil
author_facet	Badiruddeen, Nik Ahmad Khalil
author_sort	Badiruddeen, Nik Ahmad Khalil
title	Computational fluid dynamic (CFD) analysis of blended wing body (BWB) Baseline-II unmanned aerial vehicle (UAV) with canard setting angle of 10° at 0.1mach number / Nik Ahmad Khalil Badiruddeen
title_short	Computational fluid dynamic (CFD) analysis of blended wing body (BWB) Baseline-II unmanned aerial vehicle (UAV) with canard setting angle of 10° at 0.1mach number / Nik Ahmad Khalil Badiruddeen
title_full	Computational fluid dynamic (CFD) analysis of blended wing body (BWB) Baseline-II unmanned aerial vehicle (UAV) with canard setting angle of 10° at 0.1mach number / Nik Ahmad Khalil Badiruddeen
title_fullStr	Computational fluid dynamic (CFD) analysis of blended wing body (BWB) Baseline-II unmanned aerial vehicle (UAV) with canard setting angle of 10° at 0.1mach number / Nik Ahmad Khalil Badiruddeen
title_full_unstemmed	Computational fluid dynamic (CFD) analysis of blended wing body (BWB) Baseline-II unmanned aerial vehicle (UAV) with canard setting angle of 10° at 0.1mach number / Nik Ahmad Khalil Badiruddeen
title_sort	computational fluid dynamic (cfd) analysis of blended wing body (bwb) baseline-ii unmanned aerial vehicle (uav) with canard setting angle of 10° at 0.1mach number / nik ahmad khalil badiruddeen
granting_institution	Universiti Teknologi MARA (UiTM)
granting_department	Faculty of Mechanical Engineering
publishDate	2010
url	https://ir.uitm.edu.my/id/eprint/67306/1/67306.pdf
_version_	1783735676849618944

Computational fluid dynamic (CFD) analysis of blended wing body (BWB) Baseline-II unmanned aerial vehicle (UAV) with canard setting angle of 10° at 0.1mach number / Nik Ahmad Khalil Badiruddeen

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