Study of the stress-strain state of three-layer conical shells with skins made of high-modulus composite materials

1986 ◽  
Vol 21 (4) ◽  
pp. 454-459
Author(s):  
V. U. Kotel'nikov ◽  
V. A. Morozov ◽  
S. V. Mokryi ◽  
G. I. Yurin
Keyword(s):  
Composite Materials ◽  
Strain State ◽  
High Modulus ◽  
Stress Strain ◽  
Conical Shells ◽  
Stress Strain State

Experimental investigation of the stress-strain state of three-layer shells fabricated with the use of anisotropic high-modulus composite materials

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
Keyword(s):  
Experimental Investigation ◽  
Composite Materials ◽  
Strain State ◽  
High Modulus ◽  
Stress Strain ◽  
Stress Strain State

Stress-Strain State Exploration of Stringer Made of Composite Materials Depending on Layers Stacking Structure

2018 ◽  
Vol 284 ◽  
pp. 71-76
Author(s):  
P.V. Solovyev ◽  
A.I. Gomzin ◽  
L.A. Ishbulatov ◽  
S.N. Galyshev ◽  
F.F. Musin
Keyword(s):  
Composite Materials ◽  
Cross Section ◽  
Strain State ◽  
Stress Strain ◽  
Stress Strain State ◽  
Airplane Wing ◽  
External Loads ◽  
Stacking Structure ◽  
Composite Carbon ◽  
Shaped Cross Section

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.

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