ANALYTICAL MODELING AND EXPERIMENTAL VALIDATION OF LOW-VELOCITY IMPACT RESPONSES IN UNIDIRECTIONAL CFRP COMPOSITE USING FSDT AND TDOF APPROACHES.

Authors

  • ABDELMUNEM BUSHRA ABDALLA Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor, Malaysia
  • HARIS AHMAD ISRAR 1Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor, Malaysia
  • MUHAMMAD IRFAN NAUFAL ZAKI Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor, Malaysia
  • MOHD NASIR TAMIN Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor, Malaysia
  • ZAINI AHMAD Faculty of Mechanical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor, Malaysia

DOI:

https://doi.org/10.11113/jm.v48.593

Keywords:

CFRPs, low velocity impact, energy absorption, analytical model, structural integrity, CFRP, low velocity impact, energy absorption, analytical model, structural integrity

Abstract

Metallic structures have been extensively replaced with carbon fiber-reinforced polymer (CFRP) composites in many industries due to their technical advantages and design versatility. Despite these advantages, CFRP composites are sensitive to dynamic loads such as low velocity impact, which can compromise structural integrity with internal
damage. This study introduces a computationally efficient analytical model developed in MATLAB to predict impact damage in unidirectional (UD) CFRP composites, providing a faster and more cost-effective alternative to finite element simulations. The model used First Order Shear Deformation Theory (FSDT) and a Two Degrees of Freedom (TDOF) approach, incorporating a nonlinear contact force model to calculate displacements, absorbed energy and impact forces. A key novelty of this research lies in the multi-level experimental validation conducted with an Instron CEAST 9350 impact testing machine with hemispherical impactor tips at energy levels of 5.6 J, 10.3 J and 16.14 J. Results reveal that the model achieves good agreement with experimental data at lower energy levels, accurately captures the elastic behavior with a minimum error of 1%. However, the model's limitations in simulating nonlinear responses and material damage become more evident at higher energy levels, where the extent of damage has a pronounced effect on energy absorption and dissipation. This underscores the need for incorporating advanced
material models that account for damage progression and strain-rate effects to enhance accuracy and reliability. Ultimately, this work supports the development of innovative composite solutions, contributing to more efficient and cost-effective engineering practices.

References

Alshammari B. A., Alsuhybani M. S., Almushaikeh A. M., Alotaibi B. M., Alenad A. M., Alqahtani N. B. and Alharbi A. G., 2021. Comprehensive Review of the Properties and Modifications of Carbon Fiber-Reinforced Thermoplastic Composites, Polymers, 13(15): 2474

Das M., Sahu S., and Parhi D.R., 2021. Composite Materials and Their Damage Detection using AI Techniques for Aerospace Application: A Brief Review, Materials Today Proceedings, 44(1): 955-960.

Jokinen J. and Kanerva M., 2019. Simulation of Delamination Growth at CFRP-Tungsten Aerospace Laminates Using VCCT and CZM Modelling Techniques, Applied Composite Materials, 26: 709–721.

Mohammadi R., Najafabadi M.A., Saghafi H., Saeedifar M., and Zarouchas D., 2021. The Effect of Mode II Fatigue Crack Growth Rate on the Fractographic Features of CFRP Composite Laminates: An Acoustic Emission and Scanning Electron Microscopy Analysis, Engineering Fracture Mechanics, 241: 107408.

Gibson R. F. (2016). Principles of Composite Material Mechanics, CRC Press, Boca Raton, United States.

Israr H. A., Chwen T. S., Latif A. A., Wong K. J., Koloor, S. S. R., Yidris N., and Yahya M. Y., 2022. Preliminary Structural Design of Coreless Spoiler by Topological Optimization, Processes,10: 2076.

Kim J. H., Kim S. K. and Kim H. S., 2015. Enhanced Fuel Efficiency and Reduced Emissions of Aircraft Through the Use of CFRP Materials, Aerospace Science and Technology, 46: 525-531.

Johnston J. P., Koo B., Subramanian N. and Chattopadhyay A., 2017. Modeling the Molecular Structure of the Carbon Fiber/Polymer Interphase for Multiscale Analysis of Composites. Composites Part B: Engineering, 111: 27–36.

Garoz Gómez D., Pascual-González C., García-Moreno C. J. and Fernández-Blázquez J. P., 2023. Methodology to Design and Optimise Dispersed Continuous Carbon Fibre Composites Parts by Fused Filament Fabrication, Composites Part A: Applied Science and Manufacturing, 165: 107315

Li M., Zhang H., Li S., Zhu W. and Ke Y., 2022. Machine Learning and Materials Informatics Approaches for Predicting Transverse Mechanical Properties of Unidirectional CFRP Composites with Microvoids, Materials & Design, 224: 111340.

Hongkarnjanakul N., Bouvet C., and Rivallant S., 2013. Validation of low velocity impact modelling on different stacking sequences of CFRP laminates and influence of fibre failure. Composite Structures, 106: 549–559.

Bieniaś J., Jakubczak P., Surowska B. and Dragan K., 2015. Low-energy Impact Behaviour and Damage Characterization of Carbon Fibre Reinforced Polymer and Aluminium Hybrid Laminates, Archives of Civil and Mechanical Engineering, 15(4): 925–932.

Luo Z., Wang H., Ng C.T., Fu J., Zhang Z. and Wang C., 2024. On The Low-velocity Impact Properties of CFRP/HAFRP Interlayer Hybrid Fibre Composite Laminates, Engineering Structures, 315: 118387

Bianco G. D., Giammaria V., Capretti M., Boria S., Lenci S., Ciardiello R. and Castorani V., 2024. Low-Velocity Impact of Carbon, Flax, and Hybrid Composites: Performance Comparison and Numerical Modeling, Composite Structures, 344: 118318

Cengiz A., Yildirim I. M. and Avcu E., 2024. Flexural and Low Velocity Impact Behaviour of Hybrid Metal Wire Mesh/Carbon-Fibre Reinforced Epoxy Laminates, Composites Communications, 46: 101844

Hakim M. L., Nafianto R., Nugraha A. D., Wiranata A., Supriyanto E., Nugroho G. and Muflikhun M. A., 2024. Advanced FEA Simulation of GFRP and CFRP Responses to Low Velocity Impact: Exploring Impactor Diameter Variations and Damage Mechanisms, Composite Part C: Open Access, 15: 100541

Strugala G., Klugmann M., Landowski M., Szkodo M. and Mikielewicz D., 2018. A Universal NDT Method for Examination of Low Energy Impact Damage in CFRP with the Use of TLC Film, Nondestructive Testing and Evaluation. 33(3): 315–328.

Vescovini A., Li C. X., Malverti C., Jin B. C. and Manes A., 2025. Low-velocity Impact Behavior of Flat and Tapered Single–Double Composites Specimens, Composite Structures, 335: 118823

Li F., Jin S., Li W. and Luo Z., 2024. Assessment of Damage Prediction Models for Composite Laminates under Single and Repeated Low-Velocity Impacts, Aerospace Science and Technology, 155: 109633

Zhang Z., Zhang K., Zhang G. and Zheng B., 2024. Low-velocity Impact Simulation of Carbon Fiber Reinforced Composite Laminate using IFF-Criterion Based on BP-ANN, Aerospace Science and Technology, 148: 109095

Liu J., Li Y., Huang M., Zhang Y., Lu Y. and Dong L., 2024. Prediction of Low-Velocity Impact Mechanical Response and Damage in Thermoplastic Composites Considering Elastoplastic Behavior, International Journal of Impact Engineering, 194: 105099.

Li H., Li P., Li Z., Xiong J., Zhou B., Zhang H., Bai H., Wang S., Wang X., Cao H., Sun W., Han Q., Zhou J. and Guan Z., 2024. Analytical Modeling and Analysis of The Low-Velocity Penetration and Non-Penetration Behaviors of Fiber-Reinforced Composite Cylindrical Shells Based on Critical Impact Velocity Criterion, International Journal of Impact Engineering, 186: 104858.

Singh A. K., Davidson B. D., Zehnder A. T., and Hasseldine B. P. J., 2017. An Analytical Model for The Response of Carbon/epoxy-Aluminum Honeycomb Core Sandwich Structures under Quasi-Static Indentation Loading, Journal of Sandwich Structures & Materials, 21(6): 1930–1952.

Arachchige B., Ghasemnejad H. and Augousti A. T., 2016. Theoretical Approach to Predict Transverse Impact Response of Variable-Stiffness Curved Composite Plates, Composites Part B: Engineering, 89: 34–43

Salami S. J., and Dariushi S., 2018. Geometrically Nonlinear Analysis of Sandwich Beams under Low Velocity Impact: Analytical and Experimental Investigation, Steel and Composite Structures, 27(3): 273–283.

Wolniak M., Hofmeister B., Jonscher C., Fankhänel M., Loose A., Hübler C. and Rolfes R., 2023. Validation of An FE Model Updating Procedure for Damage Assessment using a Modular Laboratory Experiment with a Reversible Damage Mechanism, Journal of Civil Structural Health Monitoring, 13(6–7): 1185–1206

Ouezgan A., Mallil E. H. and Echaabi J., 2022. Manufacturing Routes of Vacuum Assisted Resin Infusion: Numerical investigation, Journal of Composite Materials, 56(21): 3221–3236.

Ameerul M., Mohsin A., Iannucci L., Greenhalgh E. S., Chirdon W., and Khattab A., 2021. Experimental and Numerical Analysis of Low-Velocity Impact of Carbon Fibre-Based Non-Crimp Fabric Reinforced Thermoplastic Composites, Polymers, 13(21): 3642

ASTM D7136/D7136M. 2007. Standard Test Method for Measuring the Damage Resistance of a Fiber- Reinforced Polymer Matrix Composite to a Drop-Weight Impact Event.

Reddy J. N., 2003. Mechanics of Laminated Composite Plates and Shells: Theory and Analysis, Second Edition, CRC Press, Boca Raton, Florida, United States

Payeganeh G. H., Ashenai Ghasemi F. and Malekzadeh K., 2010. Dynamic Response of Fiber–Metal Laminates (FMLs) Subjected to Low-Velocity Impact, Thin-Walled Structures, 48(1): 62–70.

Zhou J., Liu B., and Wang S., 2022. Finite Element Analysis on Impact Response and Damage Mechanism of Composite Laminates under Single and Repeated Low-Velocity Impact, Aerospace Science and Technology, 129: 107810

Whitney J. M., and Pagano N. J., 1970. Shear Deformation in Heterogeneous Anisotropic Plates, Journal of Applied Mechanics, 37(4): 1031–1036.

Abrate S., 2011. Impact Engineering of Composite Structures, CISM Courses and Lectures, vol. 526, Springer Wein New York, United States.

Israr H. A., Hongkarnjanakul N., Rivallant S. and Bouvet C., 2014. Post-Impact Investigation of CFRP Laminated Plate, Jurnal Teknologi, 71(2): 71-78

Bouvet C., Rivallant S. and Barrau J. J., 2012. Low Velocity Impact Modeling in Composite Laminates Capturing Permanent Indentation, Composite Science Technology, 72(16): 1977–88

He W., Guan Z. and Li X., 2013. Prediction of Permanent Indentation due to Impact on Laminated Composites Based on An Elasto-Plastic Model Incorporating Fiber Failure, Composite Structures, 96: 232–242.

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Published

2025-11-17

How to Cite

ABDALLA, A. B., ISRAR, H. A., ZAKI , M. I. N., TAMIN, M. N., & AHMAD, Z. (2025). ANALYTICAL MODELING AND EXPERIMENTAL VALIDATION OF LOW-VELOCITY IMPACT RESPONSES IN UNIDIRECTIONAL CFRP COMPOSITE USING FSDT AND TDOF APPROACHES. Jurnal Mekanikal, 48(2), 97–110. https://doi.org/10.11113/jm.v48.593

Issue

Section

Mechanical

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