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
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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 |
|---|---|
| Uncontrolled Keywords: | helicopter tail rotor propeller, quasi continuous vortex lattice method |
| Subjects: | T Technology > TJ Mechanical engineering and machinery |
| Divisions: | Mechanical Engineering |
| ID Code: | 59919 |
| Deposited By: | Haliza Zainal |
| Deposited On: | 23 Jan 2017 00:24 |
| Last Modified: | 28 Feb 2022 08:04 |
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