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Experimental study of UTM-LST generic half model transport aircraft

This paper presents the experimental results from the investigation carried out at the UTM Low Speed wind tunnel facility (UTM-LST) on a half model generic transport aircraft at several configurations of primary control surfaces (flap, aileron and elevator). The objective is to measure the aerodynam...

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Main Authors:	Ujang, M. I., Mat, S., Perumal, K., Mohd Nasir, M. N.
Format:	Conference or Workshop Item
Published:	Institute of Physics Publishing 2016
Subjects:	TJ Mechanical engineering and machinery
Online Access:	http://eprints.utm.my/id/eprint/72973/ https://www.scopus.com/inward/record.uri?eid=2-s2.0-84998774621&doi=10.1088%2f1757-899X%2f152%2f1%2f012007&partnerID=40&md5=26ad21ba7c66225e5e34cfd3fb2f0e09
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id	my.utm.72973
record_format	eprints
spelling	my.utm.729732017-11-27T02:00:04Z http://eprints.utm.my/id/eprint/72973/ Experimental study of UTM-LST generic half model transport aircraft Ujang, M. I. Mat, S. Perumal, K. Mohd Nasir, M. N. TJ Mechanical engineering and machinery This paper presents the experimental results from the investigation carried out at the UTM Low Speed wind tunnel facility (UTM-LST) on a half model generic transport aircraft at several configurations of primary control surfaces (flap, aileron and elevator). The objective is to measure the aerodynamic forces and moments due to the configuration changes. The study is carried out at two different speeds of 26.1 m/s and 43.1 m/s at corresponding Reynolds number of 1 × 106 and 2 × 106, respectively. Angle of attack of the model is varied between -2° to 20°. For the flaps, the deflection applied is 0°, 5° and 10°. Meanwhile, for aileron and elevator, the deflection applied is between -10° and 10°. The results show the differences in aerodynamic characteristics of the aircraft at different control surfaces configurations. The results obtained indicate that a laminar separation bubble developed on the surface of the wing at lower angles of attack and show that the separation process is delayed when the Reynolds number is increased. Institute of Physics Publishing 2016 Conference or Workshop Item PeerReviewed Ujang, M. I. and Mat, S. and Perumal, K. and Mohd Nasir, M. N. (2016) Experimental study of UTM-LST generic half model transport aircraft. In: 6th Innovation in Aerospace Engineering and Technology, AEROTECH 2016, 8 November 2016 through 9 November 2016, Kuala Lumpur; Malaysia. https://www.scopus.com/inward/record.uri?eid=2-s2.0-84998774621&doi=10.1088%2f1757-899X%2f152%2f1%2f012007&partnerID=40&md5=26ad21ba7c66225e5e34cfd3fb2f0e09
institution	Universiti Teknologi Malaysia
building	UTM Library
collection	Institutional Repository
continent	Asia
country	Malaysia
content_provider	Universiti Teknologi Malaysia
content_source	UTM Institutional Repository
url_provider	http://eprints.utm.my/
topic	TJ Mechanical engineering and machinery
spellingShingle	TJ Mechanical engineering and machinery Ujang, M. I. Mat, S. Perumal, K. Mohd Nasir, M. N. Experimental study of UTM-LST generic half model transport aircraft
description	This paper presents the experimental results from the investigation carried out at the UTM Low Speed wind tunnel facility (UTM-LST) on a half model generic transport aircraft at several configurations of primary control surfaces (flap, aileron and elevator). The objective is to measure the aerodynamic forces and moments due to the configuration changes. The study is carried out at two different speeds of 26.1 m/s and 43.1 m/s at corresponding Reynolds number of 1 × 106 and 2 × 106, respectively. Angle of attack of the model is varied between -2° to 20°. For the flaps, the deflection applied is 0°, 5° and 10°. Meanwhile, for aileron and elevator, the deflection applied is between -10° and 10°. The results show the differences in aerodynamic characteristics of the aircraft at different control surfaces configurations. The results obtained indicate that a laminar separation bubble developed on the surface of the wing at lower angles of attack and show that the separation process is delayed when the Reynolds number is increased.
format	Conference or Workshop Item
author	Ujang, M. I. Mat, S. Perumal, K. Mohd Nasir, M. N.
author_facet	Ujang, M. I. Mat, S. Perumal, K. Mohd Nasir, M. N.
author_sort	Ujang, M. I.
title	Experimental study of UTM-LST generic half model transport aircraft
title_short	Experimental study of UTM-LST generic half model transport aircraft
title_full	Experimental study of UTM-LST generic half model transport aircraft
title_fullStr	Experimental study of UTM-LST generic half model transport aircraft
title_full_unstemmed	Experimental study of UTM-LST generic half model transport aircraft
title_sort	experimental study of utm-lst generic half model transport aircraft
publisher	Institute of Physics Publishing
publishDate	2016
url	http://eprints.utm.my/id/eprint/72973/ https://www.scopus.com/inward/record.uri?eid=2-s2.0-84998774621&doi=10.1088%2f1757-899X%2f152%2f1%2f012007&partnerID=40&md5=26ad21ba7c66225e5e34cfd3fb2f0e09
_version_	1643656540710764544
score	13.211869

Experimental study of UTM-LST generic half model transport aircraft

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