Computational Fluids Dynamics (CFD) analysis of UiTM Blended Wing Body (BWB) Baseline-II UAV Model without Canard at Similar Reynolds and Mach Numbers with Wind Tunnel Test / Mohd Hafizi Idris

In this project paper, the aerodynamics analysis using Computational Fluid Dynamics (CFD) has been employed for Blended Wing Body (BWB) Baseline-II UAV Model without Canard at similar Reynolds and Mach numbers with wind Tunnel Test. The project was carrying out at 0.1 Mach number which is consider a...

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Main Author:	Idris, Mohd Hafizi
Format:	Thesis
Language:	English
Published:	2010
Subjects:	Management of engineering works
Online Access:	https://ir.uitm.edu.my/id/eprint/36615/1/36615.pdf
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id	my-uitm-ir.36615
record_format	uketd_dc
spelling	my-uitm-ir.366152020-11-12T04:24:40Z Computational Fluids Dynamics (CFD) analysis of UiTM Blended Wing Body (BWB) Baseline-II UAV Model without Canard at Similar Reynolds and Mach Numbers with Wind Tunnel Test / Mohd Hafizi Idris 2010 Idris, Mohd Hafizi Management of engineering works Mechanics applied to machinery. Dynamics In this project paper, the aerodynamics analysis using Computational Fluid Dynamics (CFD) has been employed for Blended Wing Body (BWB) Baseline-II UAV Model without Canard at similar Reynolds and Mach numbers with wind Tunnel Test. The project was carrying out at 0.1 Mach number which is consider at low subsonic flow. The surface drawing of BWB is modified using CATIA software to get the required body of BWB. After that, the drawing is converted to IGES format before be imported from STARCCM software. Then, the BWB models are meshed with appropriate size fiinctions. Steady-state, ideal gas, three-dimensional CFD calculations were made for the BWB model using the standard one-equation turbulence model, spalart-allmaras. Aerodynamics characteristics such as lift coefficient drag coefficient and pitching moment coefficient and pressure contours were completed at various angles of attack without canard. Subsequently, the graphs are plotted using the data obtained from the simulations. The results achieved are important in term of the stability for BWB's control system. 2010 Thesis https://ir.uitm.edu.my/id/eprint/36615/ https://ir.uitm.edu.my/id/eprint/36615/1/36615.pdf text en public degree Universiti Teknologi MARA Faculty of Mechanical Engineering Wisnoe, Wirachman (Assoc. Prof. Dr.)
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Wisnoe, Wirachman (Assoc. Prof. Dr.)
topic	Management of engineering works Management of engineering works
spellingShingle	Management of engineering works Management of engineering works Idris, Mohd Hafizi Computational Fluids Dynamics (CFD) analysis of UiTM Blended Wing Body (BWB) Baseline-II UAV Model without Canard at Similar Reynolds and Mach Numbers with Wind Tunnel Test / Mohd Hafizi Idris
description	In this project paper, the aerodynamics analysis using Computational Fluid Dynamics (CFD) has been employed for Blended Wing Body (BWB) Baseline-II UAV Model without Canard at similar Reynolds and Mach numbers with wind Tunnel Test. The project was carrying out at 0.1 Mach number which is consider at low subsonic flow. The surface drawing of BWB is modified using CATIA software to get the required body of BWB. After that, the drawing is converted to IGES format before be imported from STARCCM software. Then, the BWB models are meshed with appropriate size fiinctions. Steady-state, ideal gas, three-dimensional CFD calculations were made for the BWB model using the standard one-equation turbulence model, spalart-allmaras. Aerodynamics characteristics such as lift coefficient drag coefficient and pitching moment coefficient and pressure contours were completed at various angles of attack without canard. Subsequently, the graphs are plotted using the data obtained from the simulations. The results achieved are important in term of the stability for BWB's control system.
format	Thesis
qualification_level	Bachelor degree
author	Idris, Mohd Hafizi
author_facet	Idris, Mohd Hafizi
author_sort	Idris, Mohd Hafizi
title	Computational Fluids Dynamics (CFD) analysis of UiTM Blended Wing Body (BWB) Baseline-II UAV Model without Canard at Similar Reynolds and Mach Numbers with Wind Tunnel Test / Mohd Hafizi Idris
title_short	Computational Fluids Dynamics (CFD) analysis of UiTM Blended Wing Body (BWB) Baseline-II UAV Model without Canard at Similar Reynolds and Mach Numbers with Wind Tunnel Test / Mohd Hafizi Idris
title_full	Computational Fluids Dynamics (CFD) analysis of UiTM Blended Wing Body (BWB) Baseline-II UAV Model without Canard at Similar Reynolds and Mach Numbers with Wind Tunnel Test / Mohd Hafizi Idris
title_fullStr	Computational Fluids Dynamics (CFD) analysis of UiTM Blended Wing Body (BWB) Baseline-II UAV Model without Canard at Similar Reynolds and Mach Numbers with Wind Tunnel Test / Mohd Hafizi Idris
title_full_unstemmed	Computational Fluids Dynamics (CFD) analysis of UiTM Blended Wing Body (BWB) Baseline-II UAV Model without Canard at Similar Reynolds and Mach Numbers with Wind Tunnel Test / Mohd Hafizi Idris
title_sort	computational fluids dynamics (cfd) analysis of uitm blended wing body (bwb) baseline-ii uav model without canard at similar reynolds and mach numbers with wind tunnel test / mohd hafizi idris
granting_institution	Universiti Teknologi MARA
granting_department	Faculty of Mechanical Engineering
publishDate	2010
url	https://ir.uitm.edu.my/id/eprint/36615/1/36615.pdf
_version_	1783734348979109888

Computational Fluids Dynamics (CFD) analysis of UiTM Blended Wing Body (BWB) Baseline-II UAV Model without Canard at Similar Reynolds and Mach Numbers with Wind Tunnel Test / Mohd Hafizi Idris

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