ANALYSIS LAYER MODEL OF POLYMER COMPOSITE DESIGN UNDER MULTIFACTOR LOADING
Abstract
A mathematical model is offered for the analysis of complex stress-strain state of the layer load-carrying structures of the aircraft planes. It is presented as sets of the equations of the constraining relations of load parameters, voltages and deformation. The complex multilayered solution method that allows including specific features of the design geometry and behaviour of structural materials through multifactor loading is used for the solution of the systems of the equations.
About the Authors
Oleg G. Osyaev
Rostov Military Institute of Rocket Forces
Russian Federation
Russian Federation
Yury A. Taturin
Rostov Military Institute of Rocket Forces
Russian Federation
Russian Federation
Alexey M. Kostin
Testing Centre, Troop Unit 85907
Russian Federation
Russian Federation
Artur V. Zhukov
officer of the Post-Test Analysis Subdivision, Testing Centre, Troop Unit 85907
Russian Federation
Russian Federation
References
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3. Grigorenko Ya.M. Reshenie nelinejny`x zadach teorii obolochek na E`VM / Ya.M. Grigorenko, A.P. Mukoed. – Kiev: Vy`shha shk., 1983. – 226 s. – In Russian.
Review
For citations:
Osyaev O.G., Taturin Yu.A., Kostin A.M., Zhukov A.V. ANALYSIS LAYER MODEL OF POLYMER COMPOSITE DESIGN UNDER MULTIFACTOR LOADING. Vestnik of Don State Technical University. 2011;11(5):613-620. (In Russ.)
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