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

Ishak, Iskandar Shah and Ammoo, Mohd. Shariff and ., Firdaus and Koto, Jaswar and ., 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

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Official URL: http://isomase.org/JOMAse/Vol.7%20May%202014/7-2.p...

Abstract

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.

Item Type:Article
Subjects:A General Works
ID Code:59919
Deposited By: Haliza Zainal
Deposited On:23 Jan 2017 08:24
Last Modified:13 Jun 2017 08:32

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