An Analytical Method for Predicting Delamination Onset and Growth induced by Matrix Cracks under Quasi-Static loading

Master Thesis (2023)
Author(s)

J. Romarís Villanueva (TU Delft - Aerospace Engineering)

Contributor(s)

C Kassapoglou – Mentor (TU Delft - Aerospace Structures & Computational Mechanics)

Saullo G.P. Pereira Castro – Graduation committee member (TU Delft - Aerospace Structures & Computational Mechanics)

Rene Alderiesten – Graduation committee member (TU Delft - Structural Integrity & Composites)

Faculty
Aerospace Engineering
Copyright
© 2023 Javier Romaris Villanueva
More Info
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Publication Year
2023
Language
English
Copyright
© 2023 Javier Romaris Villanueva
Graduation Date
31-08-2023
Awarding Institution
Delft University of Technology
Programme
['Aerospace Engineering']
Faculty
Aerospace Engineering
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Abstract

An analytical model for the onset and growth of delaminations induced by matrix cracks under static loading is proposed. The model introduces four distinct configurations of delaminations originating from crack tips, which are applicable to cross-ply and general symmetrical laminates subjected to tension or tension + shear.

The delamination onset method employs Kassapoglou & Socci’s analytical crack propagation model to describe matrix cracks within the laminate. This leads to closed-form expressions for the Strain Energy Release Rate associated with both crack propagation and the initiation of delaminations at crack tips. Both expressions are used to predict the delamination onset load and crack spacing. Predictions show excellent agreement with test results for cross-plies under
tension.

Regarding the delamination growth model, it assumes a constant distance between cracks during growth (crack saturation). Experimentally-obtained Mode II interlaminar fracture toughness equation and closed-form expressions for Strain Energy Release Rate for delamination growth are employed for predictions. The model overpredicts the initial delamination length but exhibits satisfactory agreement with test results for the delamination growth in cross-ply laminates under tension.

Combining all 3 models allows for a comprehensive prediction of crack propagation, delamination onset and delamination growth for general symmetrical laminates. This comprehensive approach enables the visualization of all relevant information in a single figure, providing a concise and informative representation of the damage processes. Moreover, the analytical model facilitates the construction of design curves to investigate delamination onset in detail.

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