Abstract The possibility of estimating the fatigue life of aircraft structure at early stages of its design is considered. The assessment is performed based on a series of numerical experiments as well as the kinematic analysis and algorithms to search for rational parameters. The analysis is performed based on the finite element and superelement methods.
On the possibility of structural fatigue properties estimation at the early stages of design analysis
Russian Aeronautics (Iz VUZ) ; 57 , 1 ; 30-36
2014-01-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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