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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| Format: | Thesis |
| Language: | English |
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2009
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| Online Access: | https://ir.uitm.edu.my/id/eprint/31242/ |
| _version_ | 1848807706025000960 |
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| author | Jundam, Mohd. Fazil |
| author_facet | Jundam, Mohd. Fazil |
| author_sort | Jundam, Mohd. Fazil |
| building | UiTM Institutional Repository |
| collection | Online Access |
| 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. |
| first_indexed | 2025-11-14T22:47:05Z |
| format | Thesis |
| id | uitm-31242 |
| institution | Universiti Teknologi MARA |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-14T22:47:05Z |
| publishDate | 2009 |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | uitm-312422022-06-08T07:48:07Z https://ir.uitm.edu.my/id/eprint/31242/ 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 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 NonPeerReviewed text en https://ir.uitm.edu.my/id/eprint/31242/1/31242.PDF Jundam, Mohd. Fazil (2009) 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) Degree thesis, thesis, Universiti Teknologi MARA Shah Alam. |
| 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 |
| 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_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_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_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 |
| topic | Mechanics of engineering. Applied mechanics |
| url | https://ir.uitm.edu.my/id/eprint/31242/ |