Assessment of several modeling strategies on the prediction of lift-drag coefficients of a NACA0012 airfoil at a moderate Reynold number

Author:

Almohammadi K.M.

Funder

Taibah University

Publisher

Elsevier BV

Subject

General Engineering

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Improved performance of k − ω SST turbulence model in predicting airfoil characteristics for a wide range of airfoil thicknesses;Journal of Physics: Conference Series;2024-06-01

2. Aerodynamic performance improvement of an airfoil using the Gurney flap and fast on–off DBD plasma actuator;The European Physical Journal Plus;2024-01-07

3. Computational analysis of a new airfoil for micro-capacity wind turbine;International Journal on Interactive Design and Manufacturing (IJIDeM);2023-07-11

4. Vibrational Resonance in a Damped Bi-harmonic Driven Mathews–Lakshmanan Oscillator;Journal of Vibration Engineering & Technologies;2023-02-25

5. Experimental and LBM analysis of medium-Reynolds number fluid flow around NACA0012 airfoil;International Journal of Numerical Methods for Heat & Fluid Flow;2023-02-13

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