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We study the vibrations of multilayer composite rod. In order to influence the definition-tion features multilayered rods, clarify the roles and forms orthotropy-layers fluctuations regarded rod of arbitrary cross section and a compressor blade Nye. The numerical results obtained for ratios compared with the results calculated by ANSYS program.

About the authors

Alibek U Nurimbetov

Moscow Aviation Institute (National Research University)

Author for correspondence.
Email: alibek_55@mail.ru

Candidate of Phys-math. Sciences, doctoral candidate of the chair “Strength of aviation and rocket-and-space structures”

Volokolamskoe shosse, 4, Moscow, Russia, 125993

Alexander A Dudchenko

Moscow Aviation Institute (National Research University)

Email: a_dudchenko@mail.ru

Doctor of technical Sciences, Professor of “Strength of aviation and rocket-and-space structures”

Volokolamskoe shosse, 4, Moscow, Russia, 125993


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Copyright (c) 2017 Nurimbetov A.U., Dudchenko A.A.

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