Asynchronous Parallelization of a CFD Solver
نویسندگان
چکیده
منابع مشابه
Verification of a CFD solver in near ground effect for aerodynamic behavior of airfoil NACA 0015
Numerical investigation was performed on NACA 0015 which is a symmetric airfoil. Pressure distribution and then lift and drag forces are verified. Changing of ground clearance was a considerable point. Also the angle of attack was changed from 0° to 10°. Pressure coefficient reaches its higher amounts on the wing lower surface when the ground clearance diminishes. Increment of the angle of atta...
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ژورنال
عنوان ژورنال: Journal of Computational Engineering
سال: 2015
ISSN: 2356-7260,2314-6443
DOI: 10.1155/2015/295393