Investigation On The Propulsive Efficiency Of The Small Uav Conceptual Design
A parametric study of low altitude small Unmanned Autonomous Vehicle (UAV) conceptual design was performed. The purpose was to estimate constraint diagram propulsive efficiency of propeller-Brushless Direct Current (BLDC) motor propulsion system at two different flight conditions with the considerat...
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| Format: | Thesis |
| Language: | English |
| Published: |
2012
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| Online Access: | http://eprints.usm.my/41889/1/KHAIRUL_IKHSAN_YAHAYA.pdf |
| _version_ | 1825834514568445952 |
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| author | Yahya, Khairul Ikhsan |
| author_facet | Yahya, Khairul Ikhsan |
| author_sort | Yahya, Khairul Ikhsan |
| collection | USM |
| description | A parametric study of low altitude small Unmanned Autonomous Vehicle (UAV) conceptual design was performed. The purpose was to estimate constraint diagram propulsive efficiency of propeller-Brushless Direct Current (BLDC) motor propulsion system at two different flight conditions with the consideration of Atmospheric Boundary Layer (ABL) turbulent effect. The lift slope and drag polar of the small UAV was obtained by simulating the airframe in FluentTM 6.3 using SST k-ω turbulence model at stall, cruise and maximum
speeds. |
| first_indexed | 2024-03-06T15:23:54Z |
| format | Thesis |
| id | usm.eprints-41889 |
| institution | Universiti Sains Malaysia |
| language | English |
| last_indexed | 2024-03-06T15:23:54Z |
| publishDate | 2012 |
| record_format | dspace |
| spelling | usm.eprints-418892019-04-12T05:26:23Z http://eprints.usm.my/41889/ Investigation On The Propulsive Efficiency Of The Small Uav Conceptual Design Yahya, Khairul Ikhsan TL500-777 Aeronautics. Aeronautical engineering A parametric study of low altitude small Unmanned Autonomous Vehicle (UAV) conceptual design was performed. The purpose was to estimate constraint diagram propulsive efficiency of propeller-Brushless Direct Current (BLDC) motor propulsion system at two different flight conditions with the consideration of Atmospheric Boundary Layer (ABL) turbulent effect. The lift slope and drag polar of the small UAV was obtained by simulating the airframe in FluentTM 6.3 using SST k-ω turbulence model at stall, cruise and maximum speeds. 2012-03 Thesis NonPeerReviewed application/pdf en http://eprints.usm.my/41889/1/KHAIRUL_IKHSAN_YAHAYA.pdf Yahya, Khairul Ikhsan (2012) Investigation On The Propulsive Efficiency Of The Small Uav Conceptual Design. Masters thesis, Universiti Sains Malaysia. |
| spellingShingle | TL500-777 Aeronautics. Aeronautical engineering Yahya, Khairul Ikhsan Investigation On The Propulsive Efficiency Of The Small Uav Conceptual Design |
| title | Investigation On The Propulsive Efficiency Of
The Small Uav Conceptual Design
|
| title_full | Investigation On The Propulsive Efficiency Of
The Small Uav Conceptual Design
|
| title_fullStr | Investigation On The Propulsive Efficiency Of
The Small Uav Conceptual Design
|
| title_full_unstemmed | Investigation On The Propulsive Efficiency Of
The Small Uav Conceptual Design
|
| title_short | Investigation On The Propulsive Efficiency Of
The Small Uav Conceptual Design
|
| title_sort | investigation on the propulsive efficiency of the small uav conceptual design |
| topic | TL500-777 Aeronautics. Aeronautical engineering |
| url | http://eprints.usm.my/41889/1/KHAIRUL_IKHSAN_YAHAYA.pdf |
| work_keys_str_mv | AT yahyakhairulikhsan investigationonthepropulsiveefficiencyofthesmalluavconceptualdesign |