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...
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Formato: | Final Year Project (FYP) |
Idioma: | English |
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2013
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Acesso em linha: | http://hdl.handle.net/10356/53561 |
_version_ | 1826130387123830784 |
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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 |