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Chaotic dynamics of a continuous and discrete generalized Ziegler pendulum 连续和离散广义齐格勒摆的混沌动力学
IF 1.9 3区 工程技术 Q3 MECHANICS Pub Date : 2024-07-05 DOI: 10.1007/s11012-024-01848-5
Stefano Disca, Vincenzo Coscia

We present analytical and numerical results on integrability and transition to chaotic motion for a generalized Ziegler pendulum, a double pendulum subject to an angular elastic potential and a follower force. Several variants of the original dynamical system, including the presence of gravity and friction, are considered, in order to analyze whether the integrable cases are preserved or not in presence of further external forces, both potential and non-potential. Particular attention is devoted to the presence of dissipative forces, that are analyzed in two different formulations. Furthermore, a study of the discrete version is performed. The analysis of periodic points, that is presented up to period 3, suggests that the discrete map associated to the dynamical system has not dense sets of periodic points, so that the map would not be chaotic in the sense of Devaney for a choice of the parameters that corresponds to a general case of chaotic motion for the original system.

我们提出了关于广义齐格勒摆(受角弹性势和随动力作用的双摆)的可整性和向混沌运动过渡的分析和数值结果。考虑了原始动力系统的几种变体,包括重力和摩擦力的存在,以分析在进一步的外力(包括势能和非势能)存在时,可积分情况是否保留。特别关注了耗散力的存在,并用两种不同的公式对其进行了分析。此外,还对离散版本进行了研究。直到周期 3 的周期点分析表明,与动力系统相关的离散映射没有密集的周期点集,因此,对于与原始系统的一般混沌运动情况相对应的参数选择,映射不会是 Devaney 意义上的混沌。
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引用次数: 0
Active design method and performance prediction of internal gear pairs with low sliding ratio 低滑动比内齿轮副的主动设计方法和性能预测
IF 1.9 3区 工程技术 Q3 MECHANICS Pub Date : 2024-07-04 DOI: 10.1007/s11012-024-01845-8
Wei Sheng, Zhengminqing Li, Xiaofeng Yu, Rongsheng Xi

Reducing relative sliding between tooth surfaces contributes to the improved reliability of gear operation. This paper presents an active design of an internal gear drive with low sliding ratio (LSR). In order to achieve a lower sliding ratio, the relationship between the sliding ratio and the contact path is established. The tooth profiles of the internal gear are determined based on a given contact path using a cubic function. Tooth interference issues arising during gear meshing and machining are systematically analyzed. Additionally, tooth profile features are illustrated through an example. The operating performance, including tooth strength and lubrication characteristics, is evaluated through a comparison with that of the traditional involute gear drive. Results indicate that the novel internal gear transmission exhibits excellent resistance to wear, bending, and lubrication performance. Finally, the rationality of the tooth profile design is validated through physical assembly.

减少齿面之间的相对滑动有助于提高齿轮运行的可靠性。本文介绍了低滑动比(LSR)内齿轮传动装置的主动设计。为了实现更低的滑动比,建立了滑动比与接触路径之间的关系。根据给定的接触路径,使用三次函数确定内齿轮的齿形。系统分析了齿轮啮合和加工过程中出现的齿干涉问题。此外,还通过实例说明了齿廓特征。通过与传统渐开线齿轮传动的比较,对包括齿强度和润滑特性在内的运行性能进行了评估。结果表明,新型内齿轮传动装置具有出色的抗磨损、抗弯曲和润滑性能。最后,通过物理装配验证了齿形设计的合理性。
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引用次数: 0
CFD simulation of a Rushton turbine stirred-tank using open-source software with critical evaluation of MRF-based rotation modeling 使用开源软件对 Rushton 涡轮搅拌罐进行 CFD 模拟,并对基于 MRF 的旋转建模进行重要评估
IF 2.7 3区 工程技术 Q3 MECHANICS Pub Date : 2024-07-03 DOI: 10.1007/s11012-024-01824-z
Alfred Reid, Riccardo Rossi, Ciro Cottini, Andrea Benassi

A critical evaluation of the impact of the Multiple Reference Frame (MRF) technique on steady RANS simulations of a Rushton turbine stirred-tank is presented. The analysis, based on the open-source software OpenFOAM, is focused on the choice of the diameter and thickness of the MRF region and on their effect on the predicted velocity field and mixing times in the tank. Five diameters of the MRF region are compared for the same operating conditions of the turbine, showing limited differences in velocity profiles, which are found in general good agreement with available experimental data. Significant differences are nonetheless found in the predicted levels of turbulence intensity within the tank, with a considerable amount of artificially generated turbulence at the boundary of the MRF region for the largest diameters. The impact of the different predictions of the turbulent field on the modeling of the mixing process in the tank is evaluated by simulating the release of a passive scalar, using the frozen-flow field hypothesis. The results show changes in mixing times up to a factor of three when comparing MRF regions of different sizes. Thus, the present investigation highlights the importance of assessing the effect of the MRF zone size on numerical results as a standard practice in RANS based simulations of stirred-tanks.

本文对多参考框架(MRF)技术对 Rushton 涡轮搅拌槽稳定 RANS 模拟的影响进行了批判性评估。分析以开源软件 OpenFOAM 为基础,重点关注 MRF 区域直径和厚度的选择及其对预测速度场和搅拌罐内混合时间的影响。在涡轮机工作条件相同的情况下,对 MRF 区域的五种直径进行了比较,结果显示速度曲线的差异有限,与现有实验数据基本吻合。然而,水箱内湍流强度的预测水平存在显著差异,最大直径的 MRF 区域边界处存在大量人工产生的湍流。利用冻结流场假设,通过模拟被动标量的释放,评估了湍流场的不同预测对水槽内混合过程建模的影响。结果表明,在比较不同大小的 MRF 区域时,混合时间的变化可达三倍。因此,本研究强调了在基于 RANS 的搅拌罐模拟中,评估 MRF 区域大小对数值结果影响的重要性。
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引用次数: 0
Hybrid film cooling geometry analysis with OpenFOAM 利用 OpenFOAM 进行混合薄膜冷却几何分析
IF 1.9 3区 工程技术 Q3 MECHANICS Pub Date : 2024-07-03 DOI: 10.1007/s11012-024-01836-9
Ilyes Belouddane, Mohammed Hamel, Azzeddine Khorsi

This paper presents a numerical investigation of the film cooling performance of a new hybrid film cooling geometry. The new hybrid concept was created to enhance the film cooling performance of gas turbine blade. The scheme consists of a converging slot hole or console with a cylindrical hole featuring a branching cylindrical hole. An analysis of the cooling performance of the advanced hybrid film cooling model was carried out across blowing ratios of (B = 0.37, 0.60, and 0.87) at a density ratio of DR=1. A numerical simulation was performed using open-source CFD software OpenFOAM. The validity of the current numerical model was evaluated for the console case, revealing excellent agreement between the numerical results and the experimental data. In this study, two distinct forms, F1 and F2, are represented with the same position variation; the SST K − ({omega }) turbulence model was selected as the turbulence model for the analysis. The results show that the hybrid concepts, including auxiliary jets, enhance film cooling efficiency by effectively dispersing coolant across downstream surfaces and reducing the impact of the counter-rotating vortex pair by improving mixing with the mainstream flow. Furthermore, the supplementary jet ensures the primary coolant jet moves beside the test surface, which results in higher effectiveness, especially at high blowing ratios.

本文对新型混合薄膜冷却几何结构的薄膜冷却性能进行了数值研究。新的混合概念旨在提高燃气轮机叶片的薄膜冷却性能。该方案由一个会聚槽孔或控制台与一个以分支圆柱孔为特征的圆柱孔组成。在密度比为 DR=1 时,对先进的混合薄膜冷却模型的冷却性能进行了分析,其吹气比分别为(B = 0.37、0.60 和 0.87)。使用开源 CFD 软件 OpenFOAM 进行了数值模拟。对控制台情况下当前数值模型的有效性进行了评估,结果显示数值结果与实验数据非常吻合。在本研究中,F1 和 F2 两种不同的形式以相同的位置变化表示;选择 SST K - ({omega } )湍流模型作为分析的湍流模型。结果表明,包括辅助射流在内的混合概念通过有效地在下游表面分散冷却剂来提高薄膜冷却效率,并通过改善与主流流的混合来减少反向旋转涡对的影响。此外,辅助喷流可确保主冷却剂喷流在测试表面旁边移动,从而提高冷却效果,尤其是在高吹气比的情况下。
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引用次数: 0
Hybrid damping control of magnetorheological semi-active suspension based on feedback linearization Kalman observer 基于反馈线性化卡尔曼观测器的磁流变半主动悬架混合阻尼控制
IF 1.9 3区 工程技术 Q3 MECHANICS Pub Date : 2024-07-01 DOI: 10.1007/s11012-024-01827-w
Yu Jiang, Ruochen Wang, Dong Sun, Renkai Ding, Lin Yang

To improve the dynamic performances of nonlinear magnetorheological (MR) semi-active suspension, a hybrid damping control (HDC) based on Kalman observer of nonlinear suspension system is proposed. Firstly, the mechanical test of MR damper is carried out, and the mechanical model of MR damper and suspension system model are established. On this basis, a feedback linearization Kalman observer (FLKO) based on differential geometry theory is designed. Then, the working modes of the MR suspension system are divided according to different driving roads. HDC is proposed to achieve the dynamic control objectives under different working modes, and genetic algorithm is used to optimize the coefficients of skyhook, groundhook and distribution. The simulation results show that the estimation accuracy of FLKO is more than 85%. Compared with passive suspension, the tire dynamic load is optimized by 15.53% on A class road, improving the road holding. On B class road, the body acceleration, suspension deflection and tire dynamic load are optimized by 2.22%, 23.76% and 1.47% respectively, optimizing the dynamic performances comprehensively. On C class road, the body acceleration is optimized by 17.69%, improving the ride comfort effectively. Finally, a test bench is built, and the test results are basically consistent with simulation, which verifies the effectiveness of the designed FLKO and HDC.

为了改善非线性磁流变(MR)半主动悬架的动态性能,提出了一种基于卡尔曼观测器的非线性悬架系统混合阻尼控制(HDC)。首先,对磁流变减振器进行了力学测试,建立了磁流变减振器力学模型和悬架系统模型。在此基础上,设计了基于微分几何理论的反馈线性化卡尔曼观测器(FLKO)。然后,根据不同的行驶道路划分了 MR 悬挂系统的工作模式。为实现不同工作模式下的动态控制目标,提出了 HDC,并利用遗传算法优化了天钩、地钩和分配系数。仿真结果表明,FLKO 的估计精度大于 85%。与被动悬架相比,在 A 级道路上,轮胎动载荷优化了 15.53%,提高了路面保持性能。在 B 级道路上,车身加速度、悬架挠度和轮胎动载荷分别优化了 2.22%、23.76% 和 1.47%,全面优化了动态性能。在 C 级道路上,车身加速度优化了 17.69%,有效改善了乘坐舒适性。最后,建立了试验台,试验结果与仿真结果基本一致,验证了所设计的 FLKO 和 HDC 的有效性。
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引用次数: 0
Dynamic characteristics of rotor system with parallel and angular misaligned involute spline coupling 带有平行和角度错位渐开线花键联轴器的转子系统的动态特性
IF 1.9 3区 工程技术 Q3 MECHANICS Pub Date : 2024-06-27 DOI: 10.1007/s11012-024-01842-x
Xueyang Miao, Dong Jiang, Xing Ai, Fujian Xu, Dahai Zhang, Qingguo Fei

Spline couplings are commonly used to transfer rotary motion in rotating structures, such as low-pressure rotor systems in dual-rotor aero-engines. The misalignment introduced by spline coupling assembly error will seriously affect the safe operation of rotor system. In this paper, a method is proposed to calculate the spline meshing stiffness under arbitrary misalignment conditions, considering the static and dynamic misalignment. The accurate meshing parameters of spline couplings under parallel and angular misalignments were determined by computing the effective meshing region of misaligned spline teeth. Furthermore, a time-varying stiffness-damping spline model is established, considering friction on the spline teeth surfaces, to derive the dynamic model of the spline-rotor system under arbitrary misalignment conditions. The Newmark-β method, in conjunction with the Newton–Raphson method, was used to solve the dynamic response of the system, and the correctness of the model was verified by experiments. Finally, the variation of spline meshing stiffness and force caused by static and dynamic misalignment is described, and the effects of parallel and angular misalignment, as well as the phase difference in unbalance, on the vibration response and self-excited vibrations are also investigated.

花键联轴器通常用于传递旋转结构中的旋转运动,例如双转子航空发动机中的低压转子系统。花键联轴器装配误差带来的不对中将严重影响转子系统的安全运行。本文提出了一种计算任意不对中条件下花键啮合刚度的方法,考虑了静态和动态不对中。通过计算错位花键齿的有效啮合区域,确定了平行错位和角度错位下花键联轴器的精确啮合参数。此外,考虑到花键齿表面的摩擦,建立了时变刚度-阻尼花键模型,从而推导出任意错位条件下花键-转子系统的动态模型。采用 Newmark-β 法和 Newton-Raphson 法求解系统的动态响应,并通过实验验证了模型的正确性。最后,描述了静态和动态不对中引起的花键啮合刚度和力的变化,还研究了平行不对中和角度不对中以及不平衡相位差对振动响应和自激振动的影响。
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引用次数: 0
A statistical boundary for 3D rarefied flows through meshes: implementation to a new version of dsmcFoam+ and wind tunnel validation 穿过网格的三维稀流统计边界:在新版 dsmcFoam+ 中的实施和风洞验证
IF 2.7 3区 工程技术 Q3 MECHANICS Pub Date : 2024-06-26 DOI: 10.1007/s11012-024-01840-z
Tristan Staszak

The Direct Simulation Monte Carlo (DSMC) method has become a standard tool for rarefied aerodynamics and microchannel flows. However, the performance benefits of DSMC, such as adaptive grid sizes and number of particles, are constrained by the need to resolve small geometric details of mesh applications within relatively large simulation volumes. The requirement for a sufficient number of particles in even the smallest cells imposes a significant computational burden. A novel set of cyclic statistical boundary conditions is proposed to address the computational bottleneck associated with simulating micrometre-scale structures prevalent in atmospheric and space research under rarefied flow conditions. These conditions account for the geometric parameters of a geometric mesh and the angular dependency of impacting particles, aiming to alleviate the computational challenges posed by conventional approaches. Validation against wind tunnel measurements demonstrates excellent agreement for one of the implemented boundaries, able to simulate fine meshes for conditions of rocket soundings in the Mesosphere. The newly developed boundary conditions are implemented within the advanced DSMC solver, dsmcFoam+ framework. For this study, the solver is ported from OpenFOAM® version 2.4.0 to the OpenFOAM® version v2306 to leverage recent code developments, particularly in dynamic meshes, load balancing, and barycentric particle tracking. This advancement enhances the capabilities of DSMC simulations, offering improved fidelity and accuracy in capturing rarefied flow phenomena.

直接模拟蒙特卡罗(DSMC)方法已成为稀薄空气动力学和微通道流的标准工具。然而,由于需要在相对较大的模拟体积内解决网格应用的微小几何细节问题,DSMC 的性能优势(如自适应网格尺寸和粒子数量)受到了限制。即使是最小的单元也需要足够数量的粒子,这给计算带来了很大的负担。本文提出了一组新颖的循环统计边界条件,以解决在稀薄流动条件下模拟大气和空间研究中普遍存在的微米级结构时遇到的计算瓶颈。这些条件考虑了几何网格的几何参数和撞击颗粒的角度依赖性,旨在减轻传统方法带来的计算挑战。根据风洞测量结果进行的验证表明,其中一种实施的边界条件具有极佳的一致性,能够模拟中间层火箭探空条件下的精细网格。新开发的边界条件是在先进的 DSMC 求解器 dsmcFoam+ 框架内实施的。在这项研究中,求解器从 OpenFOAM® 2.4.0 版移植到 OpenFOAM® v2306 版,以充分利用最新的代码开发成果,特别是在动态网格、负载平衡和重力中心粒子跟踪方面。这一进步增强了 DSMC 模拟的能力,提高了捕捉稀流现象的保真度和准确性。
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引用次数: 0
A numerical model for total bending fatigue life estimation of carburized spur gears considering the hardness gradient and residual stress 考虑硬度梯度和残余应力的渗碳直齿轮总弯曲疲劳寿命估算数值模型
IF 1.9 3区 工程技术 Q3 MECHANICS Pub Date : 2024-06-21 DOI: 10.1007/s11012-024-01841-y
Xianshun Sun, Jun Zhao, Shaokang Song, Yongliang Lu, Huiyang Sun

The paper introduces a novel three-dimensional numerical model considering hardness gradient and residual stress to predict carburized gears’ total bending fatigue life. The crack initiation life was forecasted by the strain life method, considering hardness gradient and residual stress. Linear elastic stresses and strains in the tooth root fillet were corrected by Neuber’s rule for elastic–plastic material behavior. The tooth root area of the spur gear is segmented into layers using the thin slice method, and the fatigue properties of each layer are determined using the multilayer method. The crack propagation life was predicted by the extended finite element method (XFEM), considering hardness gradient and residual stress. Fracture surface analysis with electron microscopy determines the exact location where cracks initiate. The high-speed camera records the path and life of crack propagation. Single-tooth bending fatigue life (STBF) tests are conducted to validate the proposed model. The predicted fatigue lifetimes, failure locations, and crack propagation paths agree well with the experimental results.

本文介绍了一种考虑硬度梯度和残余应力的新型三维数值模型,用于预测渗碳齿轮的总弯曲疲劳寿命。在考虑硬度梯度和残余应力的情况下,采用应变寿命法预测了裂纹起始寿命。齿根圆角处的线性弹性应力和应变根据弹塑性材料行为的 Neuber 规则进行修正。使用薄片法将正齿轮的齿根区域划分为若干层,并使用多层法确定每一层的疲劳特性。考虑到硬度梯度和残余应力,采用扩展有限元法(XFEM)预测了裂纹扩展寿命。利用电子显微镜进行的断裂表面分析确定了裂纹产生的确切位置。高速摄像机记录了裂纹扩展的路径和寿命。进行了单齿弯曲疲劳寿命(STBF)测试,以验证所提出的模型。预测的疲劳寿命、失效位置和裂纹扩展路径与实验结果非常吻合。
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引用次数: 0
Tribo-dynamic modelling and analysis for a high-speed helical gear system with time-varying backlash and friction under Elastohydrodynamic Lubrication condition 弹性流体动力润滑条件下具有时变间隙和摩擦力的高速斜齿轮系统的三动态建模与分析
IF 1.9 3区 工程技术 Q3 MECHANICS Pub Date : 2024-06-20 DOI: 10.1007/s11012-024-01793-3
Zhibin Zheng, Hongzhi Yan, Jiangming Wu, Min Ge, Yin Zhang

High-speed gear reducers are highly sensitive to vibration and noise, especially in new-energy vehicles. Hence, the current nonlinear dynamics model of gears does not fully consider the influence of tooth microstructure on backlash and friction. This study establishes a nonlinear friction dynamics model for a high-speed helical gear system, which includes time-varying dynamic backlash and friction coefficient based on the fractal characterization of tooth roughness. Furthermore, it investigates the influence of tooth surface roughness on the dynamic performance by taking into account the interaction between friction and vibration under Elastohydrodynamic Lubrication (EHL). Theoretical simulation results show that an increase in tooth roughness leads to an overall deterioration in the dynamic performance of the helical gear system; however, local optimization can also be observed. In the case of a dynamic tooth backlash, the amplitude of displacement oscillations increases, and the number of frequencies increases; in terms of frictional coefficient, the amplitude of displacement oscillations increases, but the change is small compared with that of the dynamic tooth backlash, and the number of frequencies in the spectrum decreases. The results indicate that the proposed model can provide a reference for controlling the tooth roughness of high-speed gears.

高速齿轮减速器对振动和噪音高度敏感,尤其是在新能源汽车中。因此,目前的齿轮非线性动力学模型并未充分考虑齿面微观结构对齿隙和摩擦的影响。本研究建立了高速斜齿轮系统的非线性摩擦动力学模型,其中包括基于齿面粗糙度分形特征的时变动态齿隙和摩擦系数。此外,该模型还考虑了弹性流体动力润滑(EHL)下摩擦和振动之间的相互作用,研究了齿面粗糙度对动态性能的影响。理论模拟结果表明,齿面粗糙度的增加会导致斜齿轮系统动态性能的整体恶化;但是,也可以观察到局部优化。在动态齿隙方面,位移振荡的振幅增大,频率数增加;在摩擦系数方面,位移振荡的振幅增大,但与动态齿隙相比变化较小,频谱中的频率数减少。结果表明,所提出的模型可为控制高速齿轮的齿面粗糙度提供参考。
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引用次数: 0
Exploratory habitation vehicles with trim intrinsic control 具有微调内在控制功能的探索性居住飞行器
IF 2.7 3区 工程技术 Q3 MECHANICS Pub Date : 2024-06-19 DOI: 10.1007/s11012-024-01839-6
Andrea Manuello, Amedeo Manuello, Giuseppe Carlo Marano

Considering the space environment and its critical issues and consequent risks, the challenge is to define the way and tools with which future astronauts will be able to act, live and work in space and, in particular on the Moon and Mars, exploiting, at the state of art, knowledge of innovative science, engineering and technology. On the Moon and Mars, the most obvious environmental factors are extreme temperature fluctuations, low gravity and the virtual absence of atmosphere and magnetosphere. The health of a human body can be damaged by reduced values of gravity. Due to the reduced gravity on the Moon and Mars, human bones and muscles are unloaded and begin to weaken. It increases the risk of bone fractures and atrophied muscles for astronauts returning to Earth from prolonged missions. The magnetosphere and atmosphere on Earth shield from much of the dangerous solar and cosmic radiation. Radiation with extremely high energies can damage even living tissue. The surface of the Moon and Mars has been crushed by millions of impacts of celestial bodies such as asteroids, leaving a layer of regolith that could be very deep depending on the areas of the planets. The habitation module, described in this paper, is carried by a vehicle equipped with two pairs of compass shaped legs that act as supports for the habitation module capable of maintaining a certain controlled height with respect to the ground as well as a horizontal attitude, during the movement of the compass. A system of ropes wound on pulleys allows to control the height of the habitat with respect to the ground, control the structure in movement, descent and ascent. The habitat can also be lowered to the ground. The geometry of the shape of the pulleys, around which the ropes are wound, is determined in such a way that the habitation module remains at a certain height during the movement defined by the two compass-shaped advancement supports. The paper describes and analyzes the movement of the pulleys during the entire phase of the movement of the habitation module and their geometric shape is discussed.

考虑到空间环境及其关键问题和随之而来的风险,所面临的挑战是确定未来宇航员能够在空间,特别是在月球和火星上行动、生活和工作的方式和工具,利用最新的创新科学、工程和技术知识。在月球和火星上,最明显的环境因素是极端的温度波动、低重力以及几乎没有大气层和磁层。重力值降低会损害人体健康。由于月球和火星上的重力降低,人体骨骼和肌肉失去负荷,开始变得脆弱。这增加了执行完长期任务返回地球的宇航员骨折和肌肉萎缩的风险。地球上的磁层和大气层屏蔽了大部分危险的太阳辐射和宇宙辐射。能量极高的辐射甚至会损害生物组织。月球和火星的表面经过小行星等天体数百万次撞击的碾压,留下了一层可能很深的碎石层,具体深度取决于行星所在的区域。本文所述的居住舱由一个装有两对罗盘形支腿的飞行器运载,这两对罗盘形支腿作为居住舱的支撑,能够在罗盘运动过程中保持相对于地面的一定可控高度和水平姿态。滑轮上缠绕的绳索系统可以控制居住舱相对于地面的高度,控制结构的移动、下降和上升。栖息地还可以降到地面。绳索绕在滑轮上的几何形状是这样确定的,即在两个罗盘形前进支架确定的运动过程中,居住舱保持在一定高度。本文描述并分析了滑轮在居住舱运动的整个阶段的运动情况,并讨论了滑轮的几何形状。
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引用次数: 0
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