vortex interaction and roll-up in unsteady flow past tandem airfoils

A discrete vortex model coupled with a vortex dissipation and vortex core criteria is used to study the unsteady flow past two airfoils in configuration. the unsteady wakes of the airfoils are modeled by discrete vortices and timestepping is used to predict the individual wake shapes. the coupled flow is solved using a combined zeronormal flow boundary condition and kelvin condition which result in (2n + 2)x(2n + 2) equations. results are presented showing the effect of airfoilairfoil and airfoilwake interaction on the aerodynamic characteristics of the configuration. the effect of relative velocity, rate of pitching and phaselag are studied on airfoil performance and wake shape is predicted.