A fourth-order-accurate panel method based on spline interpolating polynomials for potential flow past a thin airfoil is presented. Numerical results are given for a symmetric airfoil at angle of attack, for which the fourth order accuracy of the method is clearly demonstrated.
A thin airfoil spline panel method / Napolitano, Michele; Vacca, Gaetano. - In: MECCANICA. - ISSN 0025-6455. - STAMPA. - 16:1(1981), pp. 30-32. [10.1007/BF02128306]
A thin airfoil spline panel method
Michele Napolitano;Gaetano Vacca
1981-01-01
Abstract
A fourth-order-accurate panel method based on spline interpolating polynomials for potential flow past a thin airfoil is presented. Numerical results are given for a symmetric airfoil at angle of attack, for which the fourth order accuracy of the method is clearly demonstrated.File in questo prodotto:
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