№1

(Volume 17)
> Volume 17 > №1 / 2011 / Pages: 145-154
Modelling of elements of designs of difficult geometry by three-dimensional finite elements
> Volume 17 > №1 / 2011 / Pages: 133-144
Analytical calculation of composite fuselage structure
> Volume 17 > №1 / 2011 / Pages: 116-132
Generalized Lagrange equations of the second kind of three-dimensional anisotropic shell theory
> Volume 17 > №1 / 2011 / Pages: 107-115
Identification of inhomogeneous characteristics of viscoelastic rods at bending vibration
> Volume 17 > №1 / 2011 / Pages: 71-90
The closed cylindrical shell under the influence of local loading
> Volume 17 > №1 / 2011 / Pages: 71-90
Mathematical modelling of thermomechanical processes in composite shells under local radiant heating
> Volume 17 > №1 / 2011 / Pages: 61-70
Comparative estimation of the fragmentation onset velocity of projectile on discrete and continuous shield
> Volume 17 > №1 / 2011 / Pages: 53-60
Features of stress condition for finite regions near to angular points of a boundary
> Volume 17 > №1 / 2011 / Pages: 30-52
On the effect of architecture, components and chemical composition to structure and properties of carbon-bearing composites
> Volume 17 > №1 / 2011 / Pages: 19-29
Structural simulation of elastic and elastoplastic properties of polymer/silicate nanocomposites under finite deformations
> Volume 17 > №1 / 2011 / Pages: 3-18
Appendix to model of porous materials deformation for calculation of granular composite effective elastic modulus
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