Lift and Drag Coefficient Map of NACA4415 Airfoil
نویسندگان
چکیده
Abstract The NACA4415 airfoil was numerically simulated with the help of Fluent software to analyze its aerodynamic characteristics. Results are acquired as follows: calculation accuracy is much higher than that XFOIL software; result SST k - ω (sstkw) turbulence model closest experimental value; within a certain range, larger Reynolds number is, lift coefficient and lift-to-drag ratio will be, smaller drag be; when angle attack less optimal attack, has influence on ratio; increases, increases slightly, applicable range for high ratios becomes smaller.
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ژورنال
عنوان ژورنال: Journal of physics
سال: 2021
ISSN: ['0022-3700', '1747-3721', '0368-3508', '1747-3713']
DOI: https://doi.org/10.1088/1742-6596/2076/1/012066