Stress-strain state and vibrations of disks of composite materials

1988 ◽  
Vol 24 (2) ◽  
pp. 260-267
Author(s):  
A. D. Lizarev
2018 ◽  
Vol 284 ◽  
pp. 71-76
Author(s):  
P.V. Solovyev ◽  
A.I. Gomzin ◽  
L.A. Ishbulatov ◽  
S.N. Galyshev ◽  
F.F. Musin

In this article the results of stress-strain state investigation for composite airplane wing stringer with different layers stacking structures are presented. As an object of research, a stringer made of composite carbon with V-shaped cross-section is considered. Due to the stress-strain state analysis of various stringer structures, the most effective structure for stringer layers stacking is selected, both in the view of providing the most rigidity and optimal perception by the stringer the field of external loads, which are most typical for the conditions of its operation.


1986 ◽  
Vol 21 (4) ◽  
pp. 454-459
Author(s):  
V. U. Kotel'nikov ◽  
V. A. Morozov ◽  
S. V. Mokryi ◽  
G. I. Yurin

1984 ◽  
Vol 19 (4) ◽  
pp. 470-475
Author(s):  
V. U. Kotel'nikov ◽  
S. V. Mokryi ◽  
I. A. Sergeev ◽  
A. A. Chernov ◽  
G. I. Yurin

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