Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
This thesis presents a study of aerodynamic of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel. This project is the continuation of previous research using Low Speed Tunnel LST and Computational Fluids Dynamics (CFD) simulation and is...
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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/36061/1/36061.pdf |
| _version_ | 1825738230459269120 |
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| author | Wan Razali, Wan Mohd Hafizan |
| author_facet | Wan Razali, Wan Mohd Hafizan |
| author_sort | Wan Razali, Wan Mohd Hafizan |
| collection | UITM |
| description | This thesis presents a study of aerodynamic of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel. This project is the continuation of previous research using Low Speed Tunnel LST and Computational Fluids Dynamics (CFD) simulation and is very important to validate the result it. This project will present the Analysis of BWB Aerodynamics at low subsonic speed. The study will focus on the aerodynamic characteristics at various angles of attack at 0.1 Mach number using wind tunnel test. The objective of this project is to obtain the aerodynamic characteristics such as lift coefficient, drag coefficient and pitching moment coefficient of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel and also to observe the quality of flow pattern around the BWB UAV at various angles of attack using flow visualization techniques. |
| first_indexed | 2024-03-06T02:30:23Z |
| format | Thesis |
| id | oai:ir.uitm.edu.my:36061 |
| institution | Universiti Teknologi MARA |
| language | English |
| last_indexed | 2024-03-06T02:30:23Z |
| publishDate | 2009 |
| record_format | dspace |
| spelling | oai:ir.uitm.edu.my:360612020-11-04T05:02:16Z https://ir.uitm.edu.my/id/eprint/36061/ Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali Wan Razali, Wan Mohd Hafizan Machinery exclusive of prime movers Machine design and drawing This thesis presents a study of aerodynamic of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel. This project is the continuation of previous research using Low Speed Tunnel LST and Computational Fluids Dynamics (CFD) simulation and is very important to validate the result it. This project will present the Analysis of BWB Aerodynamics at low subsonic speed. The study will focus on the aerodynamic characteristics at various angles of attack at 0.1 Mach number using wind tunnel test. The objective of this project is to obtain the aerodynamic characteristics such as lift coefficient, drag coefficient and pitching moment coefficient of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel and also to observe the quality of flow pattern around the BWB UAV at various angles of attack using flow visualization techniques. 2009 Thesis NonPeerReviewed text en https://ir.uitm.edu.my/id/eprint/36061/1/36061.pdf Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali. (2009) Degree thesis, thesis, Universiti Teknologi MARA. |
| spellingShingle | Machinery exclusive of prime movers Machine design and drawing Wan Razali, Wan Mohd Hafizan Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali |
| title | Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali |
| title_full | Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali |
| title_fullStr | Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali |
| title_full_unstemmed | Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali |
| title_short | Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali |
| title_sort | experimental aerodynamics of blended wing body bwb unmanned aerial vehicle uav with elevator deflection of 15° and 15° using wind tunnel mach number 0 1 0 15 wan mohd hafizan wan razali |
| topic | Machinery exclusive of prime movers Machine design and drawing |
| url | https://ir.uitm.edu.my/id/eprint/36061/1/36061.pdf |
| work_keys_str_mv | AT wanrazaliwanmohdhafizan experimentalaerodynamicsofblendedwingbodybwbunmannedaerialvehicleuavwithelevatordeflectionof15and15usingwindtunnelmachnumber01015wanmohdhafizanwanrazali |