In this note a fast Cauchy integral solver and its application to the solution of symmetric incompressible flows, based on a quadratic thin airfoil theory, are presented. The computed velocity near the leading edge has been corrected with the Lighthill rule. Some results relative to airfoils and to cascade are reported.
A numerical method for second order thin airfoil theory / Fortunato, Bernardo. - In: MECCANICA. - ISSN 0025-6455. - STAMPA. - 20:2(1985), pp. 171-175. [10.1007/BF02337637]
A numerical method for second order thin airfoil theory
Bernardo Fortunato
1985-01-01
Abstract
In this note a fast Cauchy integral solver and its application to the solution of symmetric incompressible flows, based on a quadratic thin airfoil theory, are presented. The computed velocity near the leading edge has been corrected with the Lighthill rule. Some results relative to airfoils and to cascade are reported.File in questo prodotto:
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