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.
