Abstract A technique for choosing a rational load-carrying scheme and weight analysis at the early stages of designing lifting surfaces with the use of a special model of the finite element method is proposed. The distribution of structure loads is determined with regard for its deformation. The numerical example is presented.
Structural optimization of lifting surfaces with regard to static aeroelasticity
Russian Aeronautics (Iz VUZ) ; 51 , 2 ; 109-113
2008-06-01
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Structural optimization of lifting surfaces with regard to static aeroelasticity
Online Contents | 2008
|On structural optimization with aeroelasticity constraints
Tema Archiv | 1994
|Aeroelasticity of two-dimensional lifting surfaces via indicial function approach
Online Contents | 2002
|Static Aeroelasticity and Flutter
Wiley | 2014
|STATIC AEROELASTICITY - A REAPPRAISAL
AIAA | 1965
|