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

Bernardo Fortunato
1985

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.
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Utilizza questo identificativo per citare o creare un link a questo documento: http://hdl.handle.net/11589/7815
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