Unsteady Transition Studies over a Pitching Airfoil Using a k-ω-γ Transition Model

Liu Jian; Xiao Zhixiang; Fu Song

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Unsteady Transition Studies over a Pitching Airfoil Using a k-ω-γ Transition Model

机译：使用k-ω-γ过渡模型对俯仰翼型进行非稳态过渡研究

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来源
《AIAA Journal》 |2018年第9期|3776-3781|共6页
作者
Liu Jian; Xiao Zhixiang; Fu Song;
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作者单位

Tsinghua Univ, Sch Aerosp Engn, Beijing 100084, Peoples R China;

Tsinghua Univ, Sch Aerosp Engn, Beijing 100084, Peoples R China;

Tsinghua Univ, Sch Aerosp Engn, Beijing 100084, Peoples R China;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
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Unsteady Transition Studies over a Pitching Airfoil Using a k-ω-γ Transition Model

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