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Open Access

Theoretical prediction, simulation and test validation of ultimate turning radius for prepregs in variable angle placement

Xianzhao XIAa, Lei ZUa,b( ), Guiming ZHANGa,b, Helin PANa( ), Qian ZHANGa,b, Jianhui FUa, Qiaoguo WUc, Lichuan ZHOUa, Zhihai BIa, Honghao LIUa
School of Mechanical Engineering, Hefei University of Technology, Hefei 230009, China
Anhui Province Key Laboratory of Aerospace Structural Parts Forming Technology and Equipment, Hefei University of Technology, Hefei 230009, China
College of Civil Engineering, Hefei University of Technology, Hefei 230009, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

The planar force model of prepreg, initially established based on the principle of minimum potential energy and the Rayleigh-Ritz method, was improved by considering the difference between the tensile and compressive moduli in the direction of the prepreg fibers. Compressive-tensile stress distribution coefficients were also established. Combined with tests on the effect of process parameters on interlayer tack, a theoretical prediction model for the turning radius related to process parameters was developed, and the impact of prepreg interlayer tack force on the minimum turning radius was analyzed. A finite element simulation model for prepreg curve placement was created to study the size and distribution patterns of folds generated during the prepreg turning process. A minimum turning radius test was conducted to establish evaluation criteria for surface defects in curve placement and verify the accuracy of the minimum turning radius prediction model. Based on this, a prediction method for the minimum turning radius of prepreg related to process parameters was established, providing constraints for the trajectory design of variable-stiffness placement composites.

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Chinese Journal of Aeronautics

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Cite this article:
XIA X, ZU L, ZHANG G, et al. Theoretical prediction, simulation and test validation of ultimate turning radius for prepregs in variable angle placement. Chinese Journal of Aeronautics, 2026, 39(1). https://doi.org/10.1016/j.cja.2025.103795

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Received: 24 October 2024
Revised: 10 December 2024
Accepted: 20 January 2025
Published: 01 September 2025
© 2025 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).