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Numerical investigations into the asymmetric effects on the aerodynamic response of a pitching airfoil

  • Xi'an Jiaotong University

科研成果: 期刊稿件 › 文章 › 同行评审

72 引用 (Scopus)

摘要

The effects of asymmetric sinusoidal motion on pitching airfoil aerodynamics were studied by numerical simulations for 2-D flow around a NACA0012 airfoil at Re = 1.35 x 105. Various unsteady parameters (amplitude of oscillation, d; reduced frequency, k) were applied to investigate the effect of asymmetry parameter S on the instantaneous force coefficients and flow patterns. The results reveal that S has a noticeable effect on the aerodynamic performance, as it affects the instantaneous force coefficient, maximum lift and drag coefficient, hysteresis loops and the flow structures

源语言英语
页(从-至)76-86
页数11
期刊Journal of Fluids and Structures
卷39
DOI
出版状态已出版 - 2013

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