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...

وصف كامل

محفوظ في:
التفاصيل البيبلوغرافية
المؤلف الرئيسي: Yahya, Khairul Ikhsan
التنسيق: أطروحة
اللغة:English
منشور في: 2012
الموضوعات:
الوصول للمادة أونلاين:http://eprints.usm.my/41889/1/KHAIRUL_IKHSAN_YAHAYA.pdf
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id my-usm-ep.41889
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spelling 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
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