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Russian Aeronautics

, Volume 59, Issue 4, pp 460–465 | Cite as

Development and verification of an analytic technique to determine the stiffness parameters of braided tubular parts

  • S. A. Samipur
  • Ya. S. DanilovEmail author
Structural Mechanics and Strength of Flight Vehicles
  • 23 Downloads

Abstract

This paper deals with development and verification of an analytical technique for determining the stiffness parameters of composite tubular aerospace structures manufactured by radial braiding and transfer molding.

Keywords

braided composite bi- and triaxial braiding mathematical model mechanical properties computer simulation 

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Copyright information

© Allerton Press, Inc. 2016

Authors and Affiliations

  1. 1.Tupolev Kazan National Research Technical UniversityTatarstanRussia

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