Mahamad, Firdaus and Koto, Jaswar and Ishak, Iskandar Shah and Ammoo, Mohd. Shariff (2015) Wind tunnel test on generic agusta-bell 206b helicopter tail rotor blades. Journal of Aeronautical -Science and Engineering, 1 . pp. 1-6. ISSN 2442-6407
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Official URL: https://isomase.org/JAse/Vol.1%20Feb%202015/1-1.pd...
Abstract
A low speed wind tunnel test was conducted for a full-scaled generic model of Agusta-Bell 206B helicopter tail rotor blades in the Universiti Teknologi Malaysia-Low Speed Tunnel (UTM- LST). The purpose of this paper is to conduct the experimental research for gaining information on general aerodynamics and performance characteristics of tail rotor blades. The lift and drag coefficients are examined in order to explore aerodynamic characteristics of the tail rotor blades. The present results may be useful to understand general aerodynamic characteristics and will be used in validation of the Quasi-Continuous Method (QCM) in the future.
| Item Type: | Article |
|---|---|
| Uncontrolled Keywords: | Wind Tunnel Test, Helicopter Tail Rotor Blades |
| Subjects: | T Technology > TJ Mechanical engineering and machinery |
| Divisions: | Mechanical Engineering |
| ID Code: | 60524 |
| Deposited By: | Haliza Zainal |
| Deposited On: | 24 Jan 2017 02:54 |
| Last Modified: | 10 Apr 2022 04:58 |
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