Procedure for Modeling the Transformation Process of a Corrugated Filler Unfolding on a Plane


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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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