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...
| Main Authors: | , , , |
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| Format: | Conference or Workshop Item |
| Published: |
2015
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| Subjects: |