Procedure for Modeling the Transformation Process of a Corrugated Filler Unfolding on a Plane
- Авторы: Zakirov I.M.1, Alekseev K.A.1, Faizullina N.M.1
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Учреждения:
- Kazan National Research Technical University
- Выпуск: Том 46, № 6 (2017)
- Страницы: 579-581
- Раздел: Reliability, Strength, and Wear Resistance of Machines and Structures
- URL: https://journal-vniispk.ru/1052-6188/article/view/193649
- DOI: https://doi.org/10.3103/S1052618817060164
- ID: 193649
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Аннотация
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.
Об авторах
I. Zakirov
Kazan National Research Technical University
Автор, ответственный за переписку.
Email: nk111286@mail.ru
Россия, Kazan
K. Alekseev
Kazan National Research Technical University
Email: nk111286@mail.ru
Россия, Kazan
N. Faizullina
Kazan National Research Technical University
Email: nk111286@mail.ru
Россия, Kazan
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