Procedure for Modeling the Transformation Process of a Corrugated Filler Unfolding on a Plane
- Authors: Zakirov I.M.1, Alekseev K.A.1, Faizullina N.M.1
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Affiliations:
- Kazan National Research Technical University
- Issue: Vol 46, No 6 (2017)
- Pages: 579-581
- Section: Reliability, Strength, and Wear Resistance of Machines and Structures
- URL: https://journals.rcsi.science/1052-6188/article/view/193649
- DOI: https://doi.org/10.3103/S1052618817060164
- ID: 193649
Cite item
Abstract
During the projection of corrugated fillers for honeycomb panels, which are widespread in the aircraft industry, the machine industry, and other industries, the problem of modeling the transformation process of this filler in space upon the change of its particular geometric parameters is relevant. There are various approaches to designing kinematic models of fillers; however, all recent procedures are labor-intensive and hardly adaptable to specific types of fillers; for this reason, the development of a universal procedure is considered.
About the authors
I. M. Zakirov
Kazan National Research Technical University
Author for correspondence.
Email: nk111286@mail.ru
Russian Federation, Kazan
K. A. Alekseev
Kazan National Research Technical University
Email: nk111286@mail.ru
Russian Federation, Kazan
N. M. Faizullina
Kazan National Research Technical University
Email: nk111286@mail.ru
Russian Federation, Kazan
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