Design procedure of factor of rigidity of aviation elastic elements

Abstract


In work the design procedure of factor of rigidity of an elastic element of type of "the squirrel wheel» is resulted. The given technique allows to raise essentially accuracy of calculations of the elastic elements applied in aviation engines.


About the authors

I. S. Barmanov

Samara State Aerospace University

Author for correspondence.
Email: isbarmanov@mail.ru

Russian Federation

Candidate of Technical Sciences

Assistant

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