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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2009
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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 |