非旋转对称月球尘埃粒子的弹塑性接触力和变形建模

IF 3.1 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE Acta Astronautica Pub Date : 2024-10-23 DOI:10.1016/j.actaastro.2024.10.059
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引用次数: 0

摘要

月球尘埃粒子的尖锐形态特征会在与材料表面接触时产生巨大的弹塑性接触力和变形,从而严重影响月球尘埃粒子的机械特性,包括其接触、碰撞、粘附、传输和磨损特性。尽管存在这些严重影响,但目前还缺乏考虑典型尖锐特征月球尘埃粒子接触特性的有效模型。本研究针对呈现典型尖锐特征的非旋转对称月球尘埃粒子,提出了一种弹塑性接触模型。研究还详细推导了月球尘埃粒子在粘附条件下与弹性和弹塑性半空间建立法向接触时观察到的各种物理反应的表达式。其中包括弹性力、弹塑性力、接触面积、拉脱力、残余位移和塑性变形面积的推导。此外,还推导了月球尘埃粒子切向加载时的切向拉脱力,并探讨了切向接触特性。将所建模型的结果与之前的实验结果进行比较后发现,所建模型在最大压痕深度和残余位移方面的误差分别仅为 6.06 % 和 1.03 %。这些误差大大低于传统球形模型的误差(分别为 60.30 % 和 60.13 %),证实了所提出模型的卓越精度。此外,还采用离散元方法分析了法向和切向接触、动态特性和塑性变形对所考虑的月球尘埃粒子的影响。分析结果与现有的接触模型进行了比较。结果显示,正常接触条件下的最大弹塑性力与初始速度呈正相关,但与横向角度呈负相关。此外,切向拉脱力与法向力和表面能呈正相关。此外,月球尘埃粒子的接触持续时间与其初速度呈正相关,而残余位移则呈负相关。例如,当初始速度从 10 m/s 增加到 50 m/s 时,最大弹塑性力从 37.64 mN 增加到 321.72 mN。将所提出的模型与其他接触模型进行比较后发现,弹性三角形金字塔模型的最大弹塑性力仅为圆柱形模型的 14.93%,球形模型的 34.23%,圆锥形模型的 76.27%,这表明由于具有典型尖锐特征的颗粒发生塑性变形,最大弹塑性力显著降低。总之,本研究的结果为非球形月球尘埃粒子在各种接触条件(如弹塑性接触和粘着接触)下的力学特性提供了重要的启示,可为月球表面的原地资源利用和飞船着陆提供指导。
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Modeling the elastic–plastic contact forces and deformations of nonrotationally symmetric lunar dust particles
The sharp morphological features of lunar dust particles generate significant elastic–plastic contact forces and deformations upon contact with material surfaces, which considerably affect the mechanical properties of lunar dust particles, including their contact, collision, adhesion, transport, and wear characteristics. Despite these severe effects, valid models considering the contact characteristics of typical sharp-featured lunar dust particles are currently lacking. This study proposes an elastic–plastic contact model for nonrotationally symmetric lunar dust particles showing typical sharp features. Detailed derivations of the expressions for various physical responses observed when lunar dust particles establish normal contacts with elastic and elastic–plastic half-spaces under adhesive conditions are also provided. These include derivations for elastic forces, elastic–plastic forces, contact areas, pull-off forces, residual displacements, and plastic deformation areas. Furthermore, the tangential pull-off force during the tangential loading of lunar dust particles is derived, and the tangential contact characteristics are explored. Comparisons of the results of the proposed model with those of previous experiments reveal that the proposed model shows errors of only 6.06 % and 1.03 % in the maximum indentation depth and residual displacement, respectively. These errors are substantially lower than those of conventional spherical models (60.30 % and 60.13 %, respectively), confirming the superior accuracy of the proposed model. Furthermore, the discrete element method is employed to analyze the effects of normal and tangential contacts, dynamic characteristics, and plastic deformations on the considered lunar dust particles. The results are then compared with those of existing contact models. They reveal that maximum elastic–plastic forces under normal contact conditions are positively correlated with the initial velocity but negatively correlated with the lateral angle. Furthermore, the tangential pull-off force is positively correlated with the normal force and surface energy. In addition, the contact duration of lunar dust particles is positively correlated with their initial velocities, while the residual displacement is negatively correlation. For instance, as the initial velocity increases from 10 to 50 m/s, the maximum elastic–plastic force increases from 37.64 to 321.72 mN. Comparisons of the proposed model with other contact models reveal that the maximum elastic–plastic force of the elastic–plastic triangular pyramid model is only 14.93 % that of the cylindrical model, 34.23 % that of the spherical model, and 76.27 % that of the conical model, indicating significant reductions in the maximum elastic–plastic force owing to the plastic deformations of particles with typical sharp features. Overall, the results of this study offer crucial insights into the mechanical characteristics of nonspherical lunar dust particles under various contact conditions, such as elastic–plastic and adhesive contacts, and can guide in situ resource utilization on the lunar surface and for craft landings.
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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