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Study of aerodynamic noise of propeller considering the influence of boundary surface using cfd method

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This article focuses on the aerodynamic and acoustic characteristics of both an isolated propeller model and a propeller - boundary surface model. The study uses the Reynoldsaveraged Navier-Stokes (RANS) method combined with Computational Fluid Dynamics techniques to analyze the flow field and wake flow behind the propeller and to determine its basic aerodynamic coefficients.

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Nội dung Text: Study of aerodynamic noise of propeller considering the influence of boundary surface using cfd method

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