Numerical Simulation of an Icebreaker Ramming the Ice Ridge

During polar navigation, icebreakers frequently encounter ice ridges, which can significantly reduce navigation efficiency and even pose threats to structural safety. Therefore, studying the ramming of ice ridges by the icebreaker is of great importance. In this study, the ice ridge is decoupled into the consolidated layer and the keel for modeling. The consolidated layer is simplified as layered ice, and an innovative hybrid empirical–numerical method is used to determine the icebreaking loads. For the keel, a failure model is developed using the Mohr–Coulomb criterion in combination with the effective stress principle, accounting for shear failure in porous media and incorporating both cohesion and internal friction angle. The ship is restricted to surge motion only. A comparative analysis with the model test results was conducted to assess the accuracy of the method, with the predicted ice resistance showing deviation of 9.85% in the consolidated ice area and 10.48% in the keel area. Ablation studies were conducted to investigate the effects of different ice ridge shapes, varying retreat distances, and different ship drafts on the performance of ramming the ice ridge. The proposed method can quickly and accurately calculate ice ridge loads and predict their motion responses, providing a suitable tool for on-site rapid navigability assessment and for the design of icebreakers.

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Institutions

Publication Details

Journal
Journal of Marine Science and Engineering
Published
2025-09-19
DOI
https://doi.org/10.3390/jmse13091815
Citations
2
Primary Topic
Spacecraft and Cryogenic Technologies
Type
article
Field-Weighted Citation Impact
9.99

Funders

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article

Numerical Simulation of an Icebreaker Ramming the Ice Ridge

Fang Li, Guangwei He, Wei Shi, Yufei Zhang et al.
2 citations
Journal of Marine Science and Engineering
Spacecraft and Cryogenic Technologies
9.99
article

Numerical Simulation of an Icebreaker Ramming the Ice Ridge

Fang Li, Guangwei He, Wei Shi, Yufei Zhang, Jiaming Chen, Wenbo Dong
article en
2 citations

Abstract

During polar navigation, icebreakers frequently encounter ice ridges, which can significantly reduce navigation efficiency and even pose threats to structural safety. Therefore, studying the ramming of ice ridges by the icebreaker is of great importance. In this study, the ice ridge is decoupled into the consolidated layer and the keel for modeling. The consolidated layer is simplified as layered ice, and an innovative hybrid empirical–numerical method is used to determine the icebreaking loads. For the keel, a failure model is developed using the Mohr–Coulomb criterion in combination with the effective stress principle, accounting for shear failure in porous media and incorporating both cohesion and internal friction angle. The ship is restricted to surge motion only. A comparative analysis with the model test results was conducted to assess the accuracy of the method, with the predicted ice resistance showing deviation of 9.85% in the consolidated ice area and 10.48% in the keel area. Ablation studies were conducted to investigate the effects of different ice ridge shapes, varying retreat distances, and different ship drafts on the performance of ramming the ice ridge. The proposed method can quickly and accurately calculate ice ridge loads and predict their motion responses, providing a suitable tool for on-site rapid navigability assessment and for the design of icebreakers.

Journal of Marine Science and EngineeringVol. 13(9)
Shanghai Jiao Tong University (CN), Shanghai Shipbuilding Technology Research Institute (CN), Jiangsu University of Science and Technology (CN), Marine Design & Research Institute of China (CN), CSSC Offshore & Marine Engineering Company (China) (CN), Shanghai Ocean University (CN)
National Natural Science Foundation of China, Science and Technology Commission of Shanghai Municipality, Ministry of Industry and Information Technology of the People's Republic of China, Young Scientists Fund, National Key Research and Development Program of China
Openalex Percentile: Top 2%
Spacecraft and Cryogenic Technologies
9.99
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