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Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method

This paper presents the Empirical Numerical Method for the analysis of the performance characteristics of a generic bell 206B helicopter tail rotor blade. The airfoil profile of the blade is near similar to NACA 0012 series, with maximum thickness 12% at 33% chord. This analysis work deals with the...

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Main Authors:	Mahamad, Firdaus, Koto, Jaswar, Ishak, Iskandar Shah, Ammoo, Mohd. Shariff
Format:	Conference or Workshop Item
Published:	2015
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://eprints.utm.my/id/eprint/61673/ https://www.science-community.org/en/node/157188
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id	my.utm.61673
record_format	eprints
spelling	my.utm.616732017-08-08T00:54:08Z http://eprints.utm.my/id/eprint/61673/ Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method Mahamad, Firdaus Koto, Jaswar Ishak, Iskandar Shah Ammoo, Mohd. Shariff TL Motor vehicles. Aeronautics. Astronautics This paper presents the Empirical Numerical Method for the analysis of the performance characteristics of a generic bell 206B helicopter tail rotor blade. The airfoil profile of the blade is near similar to NACA 0012 series, with maximum thickness 12% at 33% chord. This analysis work deals with the comparative study of variation in an angle of attack over the blade at different speed which using the software programming application that developed based on this empirical method. The analysis results were validated by comparing with the experimental results that had already done previously at Universiti Teknologi Malaysia _ Low Speed Tunnel (UTM-LST). The empirical method applied in this study was successfully able to obtain an optimal set of parameters for performance characteristics of the tail blade. 2015 Conference or Workshop Item PeerReviewed Mahamad, Firdaus and Koto, Jaswar and Ishak, Iskandar Shah and Ammoo, Mohd. Shariff (2015) Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method. In: The 2nd International Conference on Ocean, Mechanical and Aerospace., 21-22 Oct, 2015, Indonesia. https://www.science-community.org/en/node/157188
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	TL Motor vehicles. Aeronautics. Astronautics
spellingShingle	TL Motor vehicles. Aeronautics. Astronautics Mahamad, Firdaus Koto, Jaswar Ishak, Iskandar Shah Ammoo, Mohd. Shariff Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method
description	This paper presents the Empirical Numerical Method for the analysis of the performance characteristics of a generic bell 206B helicopter tail rotor blade. The airfoil profile of the blade is near similar to NACA 0012 series, with maximum thickness 12% at 33% chord. This analysis work deals with the comparative study of variation in an angle of attack over the blade at different speed which using the software programming application that developed based on this empirical method. The analysis results were validated by comparing with the experimental results that had already done previously at Universiti Teknologi Malaysia _ Low Speed Tunnel (UTM-LST). The empirical method applied in this study was successfully able to obtain an optimal set of parameters for performance characteristics of the tail blade.
format	Conference or Workshop Item
author	Mahamad, Firdaus Koto, Jaswar Ishak, Iskandar Shah Ammoo, Mohd. Shariff
author_facet	Mahamad, Firdaus Koto, Jaswar Ishak, Iskandar Shah Ammoo, Mohd. Shariff
author_sort	Mahamad, Firdaus
title	Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method
title_short	Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method
title_full	Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method
title_fullStr	Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method
title_full_unstemmed	Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method
title_sort	performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method
publishDate	2015
url	http://eprints.utm.my/id/eprint/61673/ https://www.science-community.org/en/node/157188
_version_	1643655232722305024
score	13.211869

Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method

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