Review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method

Review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method

This paper reviews on application of quasi continuous vortex lattice method for determining the performance of helicopter tail rotor propeller. Tail rotor blade for Bell B206 of one seat helicopter is used. The method is developed to be suitable for analyzing the performance of propeller in term of...

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Main Authors: Firdaus, Firdaus, Koto, Jaswar, Ammoo, Mohd. Shariff, Ishak, Iskandar Shah, Nofrizal, Nofrizal
Format: Article
Published: International Society of Ocean, Mechanical and Aerospace Scientists and Engineers 2014
Subjects:
TJ Mechanical engineering and machinery
Online Access:http://eprints.utm.my/id/eprint/59919/
http://isomase.org/JOMAse/Vol.7%20May%202014/7-2.pdf
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Institution: Universiti Teknologi Malaysia
id my.utm.59919
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spelling my.utm.599192022-02-28T08:04:56Z http://eprints.utm.my/id/eprint/59919/ Review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method Firdaus, Firdaus Koto, Jaswar Ammoo, Mohd. Shariff Ishak, Iskandar Shah Nofrizal, Nofrizal TJ Mechanical engineering and machinery This paper reviews on application of quasi continuous vortex lattice method for determining the performance of helicopter tail rotor propeller. Tail rotor blade for Bell B206 of one seat helicopter is used. The method is developed to be suitable for analyzing the performance of propeller in term of thrust, torque, and efficiency. These parameters are calculated based on pressure on blade. International Society of Ocean, Mechanical and Aerospace Scientists and Engineers 2014-05-20 Article PeerReviewed Firdaus, Firdaus and Koto, Jaswar and Ammoo, Mohd. Shariff and Ishak, Iskandar Shah and Nofrizal, Nofrizal (2014) Review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method. Journal of Ocean, Mechanical and Aerospace, Science and Engineering, 7 . pp. 8-17. ISSN 2354-7065 http://isomase.org/JOMAse/Vol.7%20May%202014/7-2.pdf
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
Firdaus, Firdaus
Koto, Jaswar
Ammoo, Mohd. Shariff
Ishak, Iskandar Shah
Nofrizal, Nofrizal
Review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method
description This paper reviews on application of quasi continuous vortex lattice method for determining the performance of helicopter tail rotor propeller. Tail rotor blade for Bell B206 of one seat helicopter is used. The method is developed to be suitable for analyzing the performance of propeller in term of thrust, torque, and efficiency. These parameters are calculated based on pressure on blade.
format Article
author Firdaus, Firdaus
Koto, Jaswar
Ammoo, Mohd. Shariff
Ishak, Iskandar Shah
Nofrizal, Nofrizal
author_facet Firdaus, Firdaus
Koto, Jaswar
Ammoo, Mohd. Shariff
Ishak, Iskandar Shah
Nofrizal, Nofrizal
author_sort Firdaus, Firdaus
title Review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method
title_short Review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method
title_full Review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method
title_fullStr Review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method
title_full_unstemmed Review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method
title_sort review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method
publisher International Society of Ocean, Mechanical and Aerospace Scientists and Engineers
publishDate 2014
url http://eprints.utm.my/id/eprint/59919/
http://isomase.org/JOMAse/Vol.7%20May%202014/7-2.pdf
_version_ 1726791449012338688

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