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

• 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

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...