Propeller test stand / Syed Khomeini Syed Hassan and Abd Manan Abd Rahman

One of importance parameters that determine the performance of an aircraft is the characteristic of the propulsion system. In designing an aircraft that uses propellers as the propulsive device, the availability of characteristics such as thrust coefficient, power coefficient and efficiency, which c...

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Bibliographic Details
Main Authors:	Syed Hassan, Syed Khomeini, Abd Rahman, Abd Manan
Format:	Student Project
Language:	English
Published:	Faculty of Mechanical Engineering 2004
Subjects:	Aircraft Rocket propulsion. Rockets
Online Access:	http://ir.uitm.edu.my/id/eprint/21252/ http://ir.uitm.edu.my/id/eprint/21252/1/PPb_SYED%20KHOMEINI%20SYED%20HASSAN%20EM%2004_5.pdf

id	uitm-21252
recordtype	eprints
spelling	uitm-212522018-10-11T08:11:49Z http://ir.uitm.edu.my/id/eprint/21252/ Propeller test stand / Syed Khomeini Syed Hassan and Abd Manan Abd Rahman Syed Hassan, Syed Khomeini Abd Rahman, Abd Manan Aircraft Rocket propulsion. Rockets One of importance parameters that determine the performance of an aircraft is the characteristic of the propulsion system. In designing an aircraft that uses propellers as the propulsive device, the availability of characteristics such as thrust coefficient, power coefficient and efficiency, which changes with advance ratio, are important to the designer so that accurate decision can be made. Previous student have design the propeller test stand that can be used in the wind tunnel to get the propeller characteristics. We continue this project starting with calibrating the thrust and torque measurement plates and then testing in the wind-tunnel for three different types of propellers. However, when we began testing the propeller in the wind-tunnel using the propeller test stand, the data logger malfunctioned. Our advisor suggested that we have to reduce our scope of the testing to static condition. To accomplish this objective a new test stand was successfully designed and fabricated using facilities available in the Faculty of Mechanical Engineering’s Workshop. The test stand was designed for Super Stock Type-R electric motor. The maximum rotational speed of the electric motor is 7000 rpm. From the results data and the graph plotted, it shows that the thrust force is increase when the rotational speed of propeller is increase and the diameter of the propeller become larger. Faculty of Mechanical Engineering 2004 Student Project NonPeerReviewed text en http://ir.uitm.edu.my/id/eprint/21252/1/PPb_SYED%20KHOMEINI%20SYED%20HASSAN%20EM%2004_5.pdf Syed Hassan, Syed Khomeini and Abd Rahman, Abd Manan (2004) Propeller test stand / Syed Khomeini Syed Hassan and Abd Manan Abd Rahman. [Student Project] (Unpublished)
repository_type	Digital Repository
institution_category	Local University
institution	Universiti Teknologi MARA
building	UiTM Institutional Repository
collection	Online Access
language	English
topic	Aircraft Rocket propulsion. Rockets
spellingShingle	Aircraft Rocket propulsion. Rockets Syed Hassan, Syed Khomeini Abd Rahman, Abd Manan Propeller test stand / Syed Khomeini Syed Hassan and Abd Manan Abd Rahman
description	One of importance parameters that determine the performance of an aircraft is the characteristic of the propulsion system. In designing an aircraft that uses propellers as the propulsive device, the availability of characteristics such as thrust coefficient, power coefficient and efficiency, which changes with advance ratio, are important to the designer so that accurate decision can be made. Previous student have design the propeller test stand that can be used in the wind tunnel to get the propeller characteristics. We continue this project starting with calibrating the thrust and torque measurement plates and then testing in the wind-tunnel for three different types of propellers. However, when we began testing the propeller in the wind-tunnel using the propeller test stand, the data logger malfunctioned. Our advisor suggested that we have to reduce our scope of the testing to static condition. To accomplish this objective a new test stand was successfully designed and fabricated using facilities available in the Faculty of Mechanical Engineering’s Workshop. The test stand was designed for Super Stock Type-R electric motor. The maximum rotational speed of the electric motor is 7000 rpm. From the results data and the graph plotted, it shows that the thrust force is increase when the rotational speed of propeller is increase and the diameter of the propeller become larger.
format	Student Project
author	Syed Hassan, Syed Khomeini Abd Rahman, Abd Manan
author_facet	Syed Hassan, Syed Khomeini Abd Rahman, Abd Manan
author_sort	Syed Hassan, Syed Khomeini
title	Propeller test stand / Syed Khomeini Syed Hassan and Abd Manan Abd Rahman
title_short	Propeller test stand / Syed Khomeini Syed Hassan and Abd Manan Abd Rahman
title_full	Propeller test stand / Syed Khomeini Syed Hassan and Abd Manan Abd Rahman
title_fullStr	Propeller test stand / Syed Khomeini Syed Hassan and Abd Manan Abd Rahman
title_full_unstemmed	Propeller test stand / Syed Khomeini Syed Hassan and Abd Manan Abd Rahman
title_sort	propeller test stand / syed khomeini syed hassan and abd manan abd rahman
publisher	Faculty of Mechanical Engineering
publishDate	2004
url	http://ir.uitm.edu.my/id/eprint/21252/ http://ir.uitm.edu.my/id/eprint/21252/1/PPb_SYED%20KHOMEINI%20SYED%20HASSAN%20EM%2004_5.pdf
first_indexed	2023-09-18T23:06:11Z
last_indexed	2023-09-18T23:06:11Z
_version_	1777418498309357568

Propeller test stand / Syed Khomeini Syed Hassan and Abd Manan Abd Rahman

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