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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my-usm-ep.418892019-04-12T05:26:23Z Investigation On The Propulsive Efficiency Of The Small Uav Conceptual Design 2012-03 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 http://eprints.usm.my/41889/ http://eprints.usm.my/41889/1/KHAIRUL_IKHSAN_YAHAYA.pdf application/pdf en public masters Universiti Sains Malaysia Pusat Pengajian Kejuteraan Aeroangkasa |
| institution |
Universiti Sains Malaysia |
| collection |
USM Institutional Repository |
| language |
English |
| topic |
TL500-777 Aeronautics Aeronautical engineering |
| spellingShingle |
TL500-777 Aeronautics Aeronautical engineering Yahya, Khairul Ikhsan Investigation On The Propulsive Efficiency Of The Small Uav Conceptual Design |
| 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. |
| format |
Thesis |
| qualification_level |
Master's degree |
| author |
Yahya, Khairul Ikhsan |
| author_facet |
Yahya, Khairul Ikhsan |
| author_sort |
Yahya, Khairul Ikhsan |
| title |
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_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_sort |
investigation on the propulsive efficiency of
the small uav conceptual design |
| granting_institution |
Universiti Sains Malaysia |
| granting_department |
Pusat Pengajian Kejuteraan Aeroangkasa |
| publishDate |
2012 |
| url |
http://eprints.usm.my/41889/1/KHAIRUL_IKHSAN_YAHAYA.pdf |
| _version_ |
1747820989747560448 |