Determination of Parameters and Verification of the Model for the Thermoforming Process of Polypropylene-Based Carbon Fiber-Reinforced Plastic

A set of input parameters for carbon fiber-reinforced plastic, required to build a computational model of a consolidated plate in the ESI PAM-FORM software, was defined. The results of measuring these characteristics, including test data obtained in the absence of standards, are presented. Based on the acquired material input parameters, calculations of fiber shear angles and thickness variation of the product during thermoforming were performed. Distribution maps of thickness and reinforcement angles, obtained from simulations of the “double dome” test specimen, are provided. Verification of the computational model was conducted by comparing the fiber shear angles derived from simulations with those measured on the physical specimen using the Apodius machine vision system.

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Publication Details

Journal
Russian Aeronautics
Published
2025-03-01
DOI
https://doi.org/10.3103/s1068799825010155
Primary Topic
Mechanical Behavior of Composites
Type
article
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article

Determination of Parameters and Verification of the Model for the Thermoforming Process of Polypropylene-Based Carbon Fiber-Reinforced Plastic

D. A. Balkaev, Л. М. Амирова, R. I. Solov’ev, I. V. Ledyaev
Russian Aeronautics
Mechanical Behavior of Composites
article

Determination of Parameters and Verification of the Model for the Thermoforming Process of Polypropylene-Based Carbon Fiber-Reinforced Plastic

D. A. Balkaev, Л. М. Амирова, R. I. Solov’ev, I. V. Ledyaev
article en

Abstract

A set of input parameters for carbon fiber-reinforced plastic, required to build a computational model of a consolidated plate in the ESI PAM-FORM software, was defined. The results of measuring these characteristics, including test data obtained in the absence of standards, are presented. Based on the acquired material input parameters, calculations of fiber shear angles and thickness variation of the product during thermoforming were performed. Distribution maps of thickness and reinforcement angles, obtained from simulations of the “double dome” test specimen, are provided. Verification of the computational model was conducted by comparing the fiber shear angles derived from simulations with those measured on the physical specimen using the Apodius machine vision system.

Russian AeronauticsVol. 68(1)
Kazan Federal University (RU), Kazan State Technical University named after A. N. Tupolev (RU)
Openalex Percentile: Top 82%
Mechanical Behavior of Composites
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