Deformation and failure of steel VNS25 at low temperatures taking account of the form of stressed state and stress concentrations

1989 ◽  
Vol 21 (1) ◽  
pp. 56-59
Author(s):  
B. I. Koval'chuk ◽  
V. N. Rudenko ◽  
A. M. Khvatan ◽  
A. A. Belous

1969 ◽  
Vol 1 (6) ◽  
pp. 621-626
Author(s):  
V. P. Lamashevskii ◽  
A. A. Lebedev ◽  
N. V. Novikov


1987 ◽  
Vol 23 (3) ◽  
pp. 266-271
Author(s):  
Yu. V. Suvorova ◽  
M. B. Akhundov ◽  
V. G. Ivanov


1992 ◽  
Vol 62 (1) ◽  
pp. 2577-2579
Author(s):  
B. O. Bagrov ◽  
T. D. Vasil'eva ◽  
N. T. Gumenyuk ◽  
T. N. Nurimov ◽  
I. N. Preobrazhenskii


1977 ◽  
Vol 9 (9) ◽  
pp. 1027-1031
Author(s):  
B. I. Koval'chuk ◽  
N. M. Kul'chitskii ◽  
A. A. Lebedev


2018 ◽  
Vol 39 (12) ◽  
pp. 1309-1318 ◽  
Author(s):  
Graeme Ewan Glass ◽  
Robert M T Staruch ◽  
Julia Ruston ◽  
Charles A East ◽  
P J Tan

AbstractRhinoplasty utilizes cartilage harvested from the nasal septum as autologous graft material. Traditional dogma espouses preservation of the “L-strut” of dorsal and caudal septum, which is less resistant to axial loading than virgin septum. Considering the 90° angle between dorsal and caudal limbs, the traditional L-strut also suffers from localized increases in internal stresses leading to premature septal “cracking,” structural-scale deformation, or both. Deformation and failure of the L-strut leads to nasal deviation, saddle deformity, loss of tip support, or restriction of the nasal valve. The balance between cartilage yield and structural integrity is a topographical optimization problem. Guided by finite element (FE) modelling, recent efforts have yielded important modifications including the chamfering of right-angled corners to reduce stress concentrations and the preservation of a minimum width along the inferior portion of the caudal strut. However, all existing FE studies offer simplified assumptions to make the construct easier to model. This review article highlights advances in our understanding of septal engineering and identifies areas that require more work to further refine the balance between the competing interests of graft acquisition and the maintenance of nasal structural integrity.



1972 ◽  
Vol 4 (5) ◽  
pp. 637-639 ◽  
Author(s):  
M. V. Zinov'ev ◽  
V. Ya. Il'ichev ◽  
V. A. Rykov ◽  
S. P. Savva




1977 ◽  
Vol 9 (4) ◽  
pp. 375-378
Author(s):  
B. I. Koval'chuk ◽  
A. A. Lebedev


2018 ◽  
Vol 183 ◽  
pp. 03016 ◽  
Author(s):  
Ivan Volkov ◽  
Leonid Igumnov ◽  
Svetlana Litvinchuk ◽  
Igor Vorobtsov

In the framework of mechanics of damaged media, behavior of thin-walled structures under pulsed loading is described. Account is taken of the interaction of the processes of dynamic deformation and damage accumulation, as well as of the main characteristic features of the dynamic failure process: the multi-staged character, nonlinear summation of damage, stressed state history and accumulated damage level. The chosen system of equations of thermo-plasticity describes the main effects of dynamic deformation of the material for random deformation trajectories. The equations of state are based on the notions of yield surface and the principle of gradientality of the plastic strain rate vector. Evolutionary equations of damage accumulation are written for a scalar parameter of damage level and are based on energy principles. The effect of the stressed state type and the accumulated damage level on the processes of nucleation, growth and merging of microdefects is accounted for. Results of numerically modelling processes of dynamic deformation and failure of spherical and closed cylindrical shells with plane and hemispherical bottoms under single pulsed explosive loading are presented. The computational results are compared with experimental data.



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