Effectiveness of Large-Camber Circular Arc Airfoil at Very Low Reynolds Numbers
نویسندگان
چکیده
منابع مشابه
Computation of Airfoils at Very Low Reynolds Numbers
We discuss a new numerical scheme involving adaptive boundary conditions which allows to compute, at very low Reynolds numbers, drag and lift of airfoils with rough surfaces efficiently with great precision. As an example we present the numerical implementation for an airfoil consisting of a line segment. The solution of the NavierStokes equations is singular at the leading and the trailing edg...
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ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
سال: 2016
ISSN: 0549-3811,2189-4205
DOI: 10.2322/tjsass.59.295