HIGH-FIDELITY SIMULATIONS OF THE FLOW AROUND WINGS AT HIGH REYNOLDS NUMBERS

Proceeding of Tenth International Symposium on Turbulence and Shear Flow Phenomena Pub Date : 1900-01-01 DOI:10.1615/tsfp10.1050

R. Vinuesa, P. Negi, A. Hanifi, D. Henningson, P. Schlatter

引用次数: 2

Abstract

Reynolds-number effects in the adverse-pressure-gradient (APG) turbulent boundary layer (TBL) developing on the suction side of a NACA4412 wing section are assessed in the present work. To this end ...

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高雷诺数下机翼绕流的高保真模拟

本文研究了NACA4412机翼截面吸力侧反压力梯度湍流边界层(TBL)的雷诺数效应。为此目的……

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Proceeding of Tenth International Symposium on Turbulence and Shear Flow Phenomena

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