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The Theoretical Research for the Rotor/Fuselage Unsteady Aerodynamic Interaction Problem

Based on coupled unsteady panel/free-wake method, a universal analysis model was established, which provides a good prediction for the rotor/fuselage unsteady aerodynamic interaction. Considering the deficiencies of the traditional time-marching rotor free-wake algorithms, notably on stability and e...

詳細記述

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書誌詳細
主要な著者: Liu Dawei, Xin Ji, Huang Jun
フォーマット: Artigo
言語:Inglês
出版事項: Instituto de Aeronáutica e Espaço (IAE) 2016-08-01
シリーズ:Journal of Aerospace Technology and Management
主題:
オンライン・アクセス:https://www.jatm.com.br/jatm/article/view/686
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