Modeling The Wing To Calculate Lift Forces And It , S Distribution By “Vortex Method”

In this article we present a quick and accurate method to calculate the aerodynamic conference - that is very important for light aircrafts – we developed program depend on “VORTEX LATTIC METHODS” we calculate the distribution of local lift forces according to wing profile. in the Earle stage of designing we concrete on lifting properties of aircraft because it effects at fighting safety where these aircrafts used mechanical direct control system. for this, accurate estimation of lift and moment conferences for wings and stabilizers have very big importance. Developing The numerical tools which depend on simple and accurate module produced by “VORTEX METHOD” is very effective tools in this stages for all kind of wings.