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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主要作者: Jundam, Mohd. Fazil
格式: Thesis
語言:English
出版: 2009
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在線閱讀:https://ir.uitm.edu.my/id/eprint/31242/1/31242.PDF
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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