Numerical study of the stress-strain state of nonuniform flexible shells of revolution made of composite materials

1985 ◽  
Vol 21 (6) ◽  
pp. 585-590
Author(s):  
Ya. M. Grigorenko ◽  
A. T. Vasilenko ◽  
N. N. Kryukov
1987 ◽  
Vol 23 (8) ◽  
pp. 760-765
Author(s):  
V. V. Skopetskii ◽  
V. S. Deineka ◽  
S. I. Rybachishin

1987 ◽  
Vol 19 (11) ◽  
pp. 1567-1570
Author(s):  
N. V. Kokhanenko ◽  
Yu. V. Kokhanenko ◽  
Z. P. Ordynskaya

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

1992 ◽  
Vol 24 (5) ◽  
pp. 347-351
Author(s):  
Yu. N. Shevchenko ◽  
M. E. Babeshko ◽  
V. I. Gololobov

1990 ◽  
Vol 26 (4) ◽  
pp. 332-336
Author(s):  
Yu. N. Nemish ◽  
I. S. Sagalyuk ◽  
D. I. Chernopiskii

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