Computational study of aerodynamic performance and flow structure around NACA 23012 wing
نویسندگان
چکیده
منابع مشابه
Aerodynamic Noise Computation of the Flow Field around NACA 0012 Airfoil Using Large Eddy Simulation and Acoustic Analogy
The current study presents the results of the aerodynamic noise prediction of the flow field around a NACA 0012 airfoil at a chord-based Reynolds number of 100,000 and at 8.4 degree angle of attack. An incompressible Large Eddy Simulation (LES) turbulence model is applied to obtain the instantaneous turbulent flow field. The noise prediction is performed by the Ffowcs Williams and Hawkings (FW-...
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ژورنال
عنوان ژورنال: International Journal of Aerodynamics
سال: 2021
ISSN: 1743-5447,1743-5455
DOI: 10.1504/ijad.2021.112707