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Degree
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Post-Graduate Student, Chair of Space-Rocket Composite Designs, Bauman Moscow State Technical University
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E-mail
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ibug@mail.ru
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Location
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Moscow
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Articles
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The theoretical model and numerical method are proposed for research of thermal and mechanical actions of radiation fluxes of various physical natures on thin-walled multilayered aircraft constructions. The finite — difference scheme of the second order of accuracy for temporary and to spatial variables is used for numerical integration of the movement equations of orthotropic shell having variable thickness and uneven heating. Results of calculations obtained by the author in the developed software system are given.
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