AERODYNAMIC LOAD OF AN AIRCRAFT WITH A HIGHLY ELASTIC WING
In this article, a method for calculation of air loads of an aircraft with an elastic wing is presented.The method can predict a redistribution of air loads when the elastic wing deforms.Unlike the traditional Euler or Navier-Stokes CFD to FEM coupling, the method uses bolia outlet gent 3D panel method as a source of aerodynamic data.This makes the