The development of method of designing the load-carrying layouts of aviation constructions using the model of a body of variable density

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The method of designing the load-carrying layouts of aviation constructions is offered on the basis of special model of a finite element method (FEM), integrating the model composed of a set of load-carrying elements of structure and model of a deformed solid of variable density. The numerical example of designing of a delta wing is resulted.

Structure, finite element method, topological optimization, continuum model, body of variable density, load-carrying layout, wing

Короткий адрес: https://sciup.org/148202599

IDR: 148202599

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