Solar UAV : propulsion system : selection of motor and propeller for MALE UAV

This report examines the works of the propulsion system selection for the solar UAV and seeks to enhance the test methodology to obtain a more accurate classification of the performance of the propeller-motor combination. The theoretical sizing of the system is re-visited and a Turnigy G110 brush...

ver descrição completa

Detalhes bibliográficos
Autor principal: Tan, Adrian Seng Leong
Outros Autores: Chue Shek Ming, Randy
Formato: Final Year Project (FYP)
Idioma:English
Publicado em: 2013
Assuntos:
Acesso em linha:http://hdl.handle.net/10356/53561
_version_ 1826130387123830784
author Tan, Adrian Seng Leong
author2 Chue Shek Ming, Randy
author_facet Chue Shek Ming, Randy
Tan, Adrian Seng Leong
author_sort Tan, Adrian Seng Leong
collection NTU
description This report examines the works of the propulsion system selection for the solar UAV and seeks to enhance the test methodology to obtain a more accurate classification of the performance of the propeller-motor combination. The theoretical sizing of the system is re-visited and a Turnigy G110 brushless outrunner motor was selected in place of the AXI 5345HD/18 brushless outrunner motor. The set-up was tested in the open circuit wind tunnel with similitude and blockage corrections. The proposed test matrix cannot be test completely due to heating issues of the motor. A post analysis was carried out and improvements are suggested in relation to the propeller, motor and test set-up for future conduct of the classification tests.
first_indexed 2024-10-01T07:55:19Z
format Final Year Project (FYP)
id ntu-10356/53561
institution Nanyang Technological University
language English
last_indexed 2024-10-01T07:55:19Z
publishDate 2013
record_format dspace
spelling ntu-10356/535612023-03-04T18:40:29Z Solar UAV : propulsion system : selection of motor and propeller for MALE UAV Tan, Adrian Seng Leong Chue Shek Ming, Randy School of Mechanical and Aerospace Engineering DSO National Laboratories DRNTU::Engineering::Aeronautical engineering::Aircraft motors and engines DRNTU::Engineering::Aeronautical engineering::Propellers This report examines the works of the propulsion system selection for the solar UAV and seeks to enhance the test methodology to obtain a more accurate classification of the performance of the propeller-motor combination. The theoretical sizing of the system is re-visited and a Turnigy G110 brushless outrunner motor was selected in place of the AXI 5345HD/18 brushless outrunner motor. The set-up was tested in the open circuit wind tunnel with similitude and blockage corrections. The proposed test matrix cannot be test completely due to heating issues of the motor. A post analysis was carried out and improvements are suggested in relation to the propeller, motor and test set-up for future conduct of the classification tests. Bachelor of Engineering (Aerospace Engineering) 2013-06-05T04:32:16Z 2013-06-05T04:32:16Z 2013 2013 Final Year Project (FYP) http://hdl.handle.net/10356/53561 en Nanyang Technological University 75 p. application/pdf
spellingShingle DRNTU::Engineering::Aeronautical engineering::Aircraft motors and engines
DRNTU::Engineering::Aeronautical engineering::Propellers
Tan, Adrian Seng Leong
Solar UAV : propulsion system : selection of motor and propeller for MALE UAV
title Solar UAV : propulsion system : selection of motor and propeller for MALE UAV
title_full Solar UAV : propulsion system : selection of motor and propeller for MALE UAV
title_fullStr Solar UAV : propulsion system : selection of motor and propeller for MALE UAV
title_full_unstemmed Solar UAV : propulsion system : selection of motor and propeller for MALE UAV
title_short Solar UAV : propulsion system : selection of motor and propeller for MALE UAV
title_sort solar uav propulsion system selection of motor and propeller for male uav
topic DRNTU::Engineering::Aeronautical engineering::Aircraft motors and engines
DRNTU::Engineering::Aeronautical engineering::Propellers
url http://hdl.handle.net/10356/53561
work_keys_str_mv AT tanadriansengleong solaruavpropulsionsystemselectionofmotorandpropellerformaleuav