S. Wang, M. Jiang, J. Lin | 2025 | Advances in Space Research
DOI 10.1016/j.asr.2024.10.048Review state
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This paper discusses the impact of rubber membrane properties on the mechanical behavior of lunar regolith under low confining pressure. It introduces a discrete element method (DEM) framework incorporating Chang E-5 particle shapes and flexible boundary conditions. Topological data analysis (TDA) is used to quantify strain localization dynamics. No lunar regolith simulants are explicitly mentioned or characterized in the text. The provided text appears to be a series of URLs, likely from a scientific or technical paper hosted on a platform like Elsevier. These URLs point to supplementary materials, figures, tables, or other supporting content related to the paper. The main paper's title, authors, and abstract are not included in the text, making it difficult to provide a detailed summary. However, based on the context of the URLs, it is likely that the paper discusses topics related to lunar or planetary geology, materials science, or engineering, given the mention of 'lunar regolith' and 'simulant' in some of the URLs. The paper may explore the mechanical properties of lunar regolith or its simulants under various conditions, which is a common topic in space exploration and plane
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Chang'E-5 | strain localization analysis
DEM simulation of the grain size distribution and corresponding rolling resistance coefficient
Mechanical
Calibration of membrane bond parameter and membrane test scenarios
Mechanical
Triaxial compression testing
Geotechnical characterization | Mobility and excavation
Storage Service
Amazon S3
Sphericity
3.0.CO;2-4
Friction angle
derived from triaxial or shear-strength testing