scholarly journals Stress-Deformed State of a Packing Ring with Eccentric Holes

Author(s):  
Ilman Hasanov ◽  
Ibrahim Abbasov ◽  
Nurlan Gurbanov

AbstractCurrently, various variants of physical and geometrical non-linear calculation of anisotropic bodies have been developed. In spite of the large and increasing number of studies on the theory of shells there are still many unsufficiently developed problems important both in scientific and applied fields, for example, development of practically convenient methods for calculating of anisotropic sealing composite materials weakened by eccentric holes under the influence of local loadings. Stress-deformed state of a packing ring with eccentric holes of sealing materials was studied. In composite materials, the Hooke’s equation was used for this purpose. Also, using Lurie’s symbolic method, the concrete solution of the sealing problem with eccentric holes was obtained.

2017 ◽  
Vol 44 (9) ◽  
pp. 51-58
Author(s):  
A.V. Genis ◽  
A.V. Kuznetsov ◽  
G.M. Il'yutkina ◽  
L.V. Polyakov

The main relationships governing the production of combined filter/sorption materials by plying-up with the application of adhesive melts have been studied. It has been established that the use of single-stage bonding technology makes it possible to improve the physical and physicomechanical properties of multilayer non-woven mats. The possibility of optimising the plying-up process by using multiple non-linear regression analysis has been demonstrated. Materials with service properties suitable for use in protective clothing have been obtained.


2010 ◽  
Vol 32 (10) ◽  
pp. 1731-1738 ◽  
Author(s):  
Anastasios P. Vassilopoulos ◽  
Behzad D. Manshadi ◽  
Thomas Keller

1994 ◽  
Vol 50 (3) ◽  
pp. 355-365 ◽  
Author(s):  
Henjen Ho ◽  
John Morton ◽  
Gary L. Farley

1971 ◽  
Vol 6 (4) ◽  
pp. 469-478 ◽  
Author(s):  
Ibrahim K. Ebcioglu

Author(s):  
V. Ramamurti ◽  
S. Rajarajan ◽  
G. V. Rao

Abstract Finite element method using three noded plate and shell element and 3D beam element in conjunction with mode superposition method is used for studying the large dynamic displacement response of a typical payload fairing due to separation impulse. Incremental technique is used for solving the geometric non-linear problem. Linear formulations are assumed and a step-by-step analysis is performed on the deformed state of each previous time step. The geometry is updated and the stiffness matrix recomputed after every finite time step and the eigenvalue analysis repeated.


2020 ◽  
Vol 19 (3) ◽  
pp. 430-435
Author(s):  
Xiaolong Bai ◽  
Vitaliy Zemlyak ◽  
Alexey Vasilyev ◽  
Victor Kozin

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