Comparing the effect of three transition models on the CFD predictions of a NACA0012 airfoil aerodynamics
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- 作者：Panagiotis-Chrysovalantis S. Kapsalisa ; Spyros Voutsinasb ; Nicholas S. Vlachosa ; vlachos@uth.gr" class="auth_mail" title="E-mail the corresponding author
- 关键词：Aerodynamics ; NACA0012 airfoil ; Transition model ; CFD ; Navier&ndash ; Stokes solver
- 刊名：Journal of Wind Engineering and Industrial Aerodynamics
- 出版年：2016
- 出版时间：October 2016
- 年：2016
- 卷：157
- 期：Complete
- 页码：158-170
- 全文大小：4564 K
文摘
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Comparison of three models for predicting flow transition.
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Michel's empirical, eN, and K–V transition models.
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Transition models based on linear stability analysis.
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Effect of transition models on airfoil aerodynamic characteristics.
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Low turbulence air flow around a smooth NACA0012 airfoil.
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CAFFAeroel 2D curvilinear, aerodynamic Navier–Stokes CFD code.