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

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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Bibliographic Details
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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Institution: Universiti Teknologi Malaysia

Internet

http://eprints.utm.my/id/eprint/61673/
https://www.science-community.org/en/node/157188

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