Design, detail analysis and performance testing of uav propulsion system

This project report is being conduct because the use of an Unmanned Aerial Vehicle (UAV) is getting popular among people either to have fun or study but the choices of powerplant are not fully deployed (in term of operational and performance sizing) and thus limiting the selection. The objective of...

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Main Author:	Che Muhammad Ridhwan, Che Hashim
Format:	Undergraduates Project Papers
Language:	English English English English
Published:	2012
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://umpir.ump.edu.my/id/eprint/4470/ http://umpir.ump.edu.my/id/eprint/4470/ http://umpir.ump.edu.my/id/eprint/4470/1/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28Table%20of%20content%29.pdf http://umpir.ump.edu.my/id/eprint/4470/2/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28Abstract%29.pdf http://umpir.ump.edu.my/id/eprint/4470/3/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28Chapter%201%29.pdf http://umpir.ump.edu.my/id/eprint/4470/4/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28References%29.pdf

id	ump-4470
recordtype	eprints
spelling	ump-44702017-04-04T03:43:43Z http://umpir.ump.edu.my/id/eprint/4470/ Design, detail analysis and performance testing of uav propulsion system Che Muhammad Ridhwan, Che Hashim TL Motor vehicles. Aeronautics. Astronautics This project report is being conduct because the use of an Unmanned Aerial Vehicle (UAV) is getting popular among people either to have fun or study but the choices of powerplant are not fully deployed (in term of operational and performance sizing) and thus limiting the selection. The objective of this project is to propose a design, detail analysis and performance testing of an Unmanned Aerial Vehicle (UAV) propulsion system. In this study, the test bed model was designed to test the nitro engine Radio Control (RC) which is model of 46-LA OS Engine Series of aircraft performance which are four performance parameters that was studied such as thrust, available power and shaft brake power, propulsive efficiency and brake specific fuel consumption thus the performance parameters value can be calculated by measure the unknown value of parameters regarding to the equation involves within the range 2000 to 16000 RPM of engine speed by setting the test bed design with suitable apparatus. From this experiment, the result shows that the fabricated test bed can be use to study the engine performance and performance parameters are directly proportional to the engine speed which is mean the faster the speed of engine effected the increasing of performance parameters. As a conclusion, even without testing the engine to the real body of aircraft, all the engine performance parameter can be calculated from this experiment, and it will reduce the time and cost. 2012-06 Undergraduates Project Papers NonPeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/4470/1/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28Table%20of%20content%29.pdf application/pdf en http://umpir.ump.edu.my/id/eprint/4470/2/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28Abstract%29.pdf application/pdf en http://umpir.ump.edu.my/id/eprint/4470/3/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28Chapter%201%29.pdf application/pdf en http://umpir.ump.edu.my/id/eprint/4470/4/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28References%29.pdf Che Muhammad Ridhwan, Che Hashim (2012) Design, detail analysis and performance testing of uav propulsion system. Faculty of Mechanical Engineering, Universiti Malaysia Pahang. http://iportal.ump.edu.my/lib/item?id=chamo:69523&theme=UMP2
repository_type	Digital Repository
institution_category	Local University
institution	Universiti Malaysia Pahang
building	UMP Institutional Repository
collection	Online Access
language	English English English English
topic	TL Motor vehicles. Aeronautics. Astronautics
spellingShingle	TL Motor vehicles. Aeronautics. Astronautics Che Muhammad Ridhwan, Che Hashim Design, detail analysis and performance testing of uav propulsion system
description	This project report is being conduct because the use of an Unmanned Aerial Vehicle (UAV) is getting popular among people either to have fun or study but the choices of powerplant are not fully deployed (in term of operational and performance sizing) and thus limiting the selection. The objective of this project is to propose a design, detail analysis and performance testing of an Unmanned Aerial Vehicle (UAV) propulsion system. In this study, the test bed model was designed to test the nitro engine Radio Control (RC) which is model of 46-LA OS Engine Series of aircraft performance which are four performance parameters that was studied such as thrust, available power and shaft brake power, propulsive efficiency and brake specific fuel consumption thus the performance parameters value can be calculated by measure the unknown value of parameters regarding to the equation involves within the range 2000 to 16000 RPM of engine speed by setting the test bed design with suitable apparatus. From this experiment, the result shows that the fabricated test bed can be use to study the engine performance and performance parameters are directly proportional to the engine speed which is mean the faster the speed of engine effected the increasing of performance parameters. As a conclusion, even without testing the engine to the real body of aircraft, all the engine performance parameter can be calculated from this experiment, and it will reduce the time and cost.
format	Undergraduates Project Papers
author	Che Muhammad Ridhwan, Che Hashim
author_facet	Che Muhammad Ridhwan, Che Hashim
author_sort	Che Muhammad Ridhwan, Che Hashim
title	Design, detail analysis and performance testing of uav propulsion system
title_short	Design, detail analysis and performance testing of uav propulsion system
title_full	Design, detail analysis and performance testing of uav propulsion system
title_fullStr	Design, detail analysis and performance testing of uav propulsion system
title_full_unstemmed	Design, detail analysis and performance testing of uav propulsion system
title_sort	design, detail analysis and performance testing of uav propulsion system
publishDate	2012
url	http://umpir.ump.edu.my/id/eprint/4470/ http://umpir.ump.edu.my/id/eprint/4470/ http://umpir.ump.edu.my/id/eprint/4470/1/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28Table%20of%20content%29.pdf http://umpir.ump.edu.my/id/eprint/4470/2/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28Abstract%29.pdf http://umpir.ump.edu.my/id/eprint/4470/3/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28Chapter%201%29.pdf http://umpir.ump.edu.my/id/eprint/4470/4/Design%2C%20detail%20analysis%20and%20performance%20testing%20of%20uav%20propulsion%20system%20%28References%29.pdf
first_indexed	2023-09-18T21:59:05Z
last_indexed	2023-09-18T21:59:05Z
_version_	1777414277313855488

Design, detail analysis and performance testing of uav propulsion system

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