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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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書誌詳細
主要な著者:	Mahamad, Firdaus, Koto, Jaswar, Ishak, Iskandar Shah, Ammoo, Mohd. Shariff
フォーマット:	Conference or Workshop Item
出版事項:	2015
主題:	TL Motor vehicles. Aeronautics. Astronautics
オンライン･アクセス:	http://eprints.utm.my/id/eprint/61673/ https://www.science-community.org/en/node/157188
タグ:	タグ追加タグなし, このレコードへの初めてのタグを付けませんか!

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