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.
|Titolo:||A numerical method for second order thin airfoil theory|
|Data di pubblicazione:||1985|
|Digital Object Identifier (DOI):||http://dx.doi.org/10.1007/BF02337637|
|Appare nelle tipologie:||1.1 Articolo in rivista|