Detail experimental testing of unmanned aerial vehicles engine performance

This project is about detail experimental testing of Unmanned Aerial Vehicles (UAV) engine performance. However, there is no proper selection of test bed available for the performance evaluation, testing and analysis of the UAV propulsion system. This project has two major objectives which are to de...

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Bibliographic Details
Main Author:	Moganaraj, Murugiah
Format:	Undergraduates Project Papers
Language:	English
Published:	2013
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://umpir.ump.edu.my/id/eprint/8666/ http://umpir.ump.edu.my/id/eprint/8666/ http://umpir.ump.edu.my/id/eprint/8666/1/cd8169.pdf

id	ump-8666
recordtype	eprints
spelling	ump-86662015-11-02T01:47:29Z http://umpir.ump.edu.my/id/eprint/8666/ Detail experimental testing of unmanned aerial vehicles engine performance Moganaraj, Murugiah TL Motor vehicles. Aeronautics. Astronautics This project is about detail experimental testing of Unmanned Aerial Vehicles (UAV) engine performance. However, there is no proper selection of test bed available for the performance evaluation, testing and analysis of the UAV propulsion system. This project has two major objectives which are to design and fabricate a test bed for the UAV propulsion system and to conduct detail performance experimentations of the UAV propulsion system run at various speed. In this study, test bed model is designed to test the nitro engine Unmanned Aerial Vehicle (UAV) which is model of Thunder Tiger Pro36 Engine Series of aircraft performance. In addition, six performance parameters are recorded for testing of the engine performance, which are Thrust, shaft brake power, available power, propulsive efficiency, specific fuel consumption and thrust coefficient. Furthermore, the method used in this project is to identify the unknown variables in parameters by using some sensors. The results show that the fabricated test bed can be used to study the engine performance. Specifically, performance parameters are directly proportional to the engine speed. These results show that the performance parameters are increasing along with the speed. In conclusion, the fabricated test bed can be used for the testing of engine performance analysis. Outcomes of this experiment can be successful by using the test bed because it helps to reduce the cost and time for UAV propulsion performances testing. 2013-06 Undergraduates Project Papers NonPeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/8666/1/cd8169.pdf Moganaraj, Murugiah (2013) Detail experimental testing of unmanned aerial vehicles engine performance. Faculty of Mechanical Engineering, Universiti Malaysia Pahang. http://iportal.ump.edu.my/lib/item?id=chamo:82912&theme=UMP2
repository_type	Digital Repository
institution_category	Local University
institution	Universiti Malaysia Pahang
building	UMP Institutional Repository
collection	Online Access
language	English
topic	TL Motor vehicles. Aeronautics. Astronautics
spellingShingle	TL Motor vehicles. Aeronautics. Astronautics Moganaraj, Murugiah Detail experimental testing of unmanned aerial vehicles engine performance
description	This project is about detail experimental testing of Unmanned Aerial Vehicles (UAV) engine performance. However, there is no proper selection of test bed available for the performance evaluation, testing and analysis of the UAV propulsion system. This project has two major objectives which are to design and fabricate a test bed for the UAV propulsion system and to conduct detail performance experimentations of the UAV propulsion system run at various speed. In this study, test bed model is designed to test the nitro engine Unmanned Aerial Vehicle (UAV) which is model of Thunder Tiger Pro36 Engine Series of aircraft performance. In addition, six performance parameters are recorded for testing of the engine performance, which are Thrust, shaft brake power, available power, propulsive efficiency, specific fuel consumption and thrust coefficient. Furthermore, the method used in this project is to identify the unknown variables in parameters by using some sensors. The results show that the fabricated test bed can be used to study the engine performance. Specifically, performance parameters are directly proportional to the engine speed. These results show that the performance parameters are increasing along with the speed. In conclusion, the fabricated test bed can be used for the testing of engine performance analysis. Outcomes of this experiment can be successful by using the test bed because it helps to reduce the cost and time for UAV propulsion performances testing.
format	Undergraduates Project Papers
author	Moganaraj, Murugiah
author_facet	Moganaraj, Murugiah
author_sort	Moganaraj, Murugiah
title	Detail experimental testing of unmanned aerial vehicles engine performance
title_short	Detail experimental testing of unmanned aerial vehicles engine performance
title_full	Detail experimental testing of unmanned aerial vehicles engine performance
title_fullStr	Detail experimental testing of unmanned aerial vehicles engine performance
title_full_unstemmed	Detail experimental testing of unmanned aerial vehicles engine performance
title_sort	detail experimental testing of unmanned aerial vehicles engine performance
publishDate	2013
url	http://umpir.ump.edu.my/id/eprint/8666/ http://umpir.ump.edu.my/id/eprint/8666/ http://umpir.ump.edu.my/id/eprint/8666/1/cd8169.pdf
first_indexed	2023-09-18T22:06:29Z
last_indexed	2023-09-18T22:06:29Z
_version_	1777414742696001536

Detail experimental testing of unmanned aerial vehicles engine performance

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