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Helicopter Rotor Aerodynamic Characteristics in Ground Effect: Numerical Study

This article represents a full estimation of helicopter rotor aerodynamic characteristics in ground effect conditions through the application of a coupled empirical blade element–momentum theory algorithm. The main focus of this research includes the evaluation of the required weighted power coeffic...

詳細記述

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書誌詳細
第一著者: Gabriel Georgiev
フォーマット: Artigo
言語:Inglês
出版事項: MDPI AG 2025-07-01
シリーズ:Engineering Proceedings
主題:
オンライン・アクセス:https://www.mdpi.com/2673-4591/100/1/13
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