Email this article Development and verification of an analytic technique to determine the stiffness parameters of braided tubular parts
- Authors: Samipur S.A.1, Danilov Y.S.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 59, No 4 (2016)
- Pages: 460-465
- Section: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/229839
- DOI: https://doi.org/10.3103/S1068799816040048
- ID: 229839
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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.
About the authors
S. A. Samipur
Tupolev Kazan National Research Technical University
Email: pla.kai@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
Ya. S. Danilov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: pla.kai@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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