STRUCTURAL CHARACTERIZATION OF PBTI03, SM0.6ND0.4NIO3 AND NDMNO3 MULTIFUNCTIONAL PEROVSKITE THIN FILMS



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 Baby 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 3D panel method as a source of aerodynamic data.This makes the calculation

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