期刊文献+
共找到1,920篇文章
< 1 2 96 >
每页显示 20 50 100
Analytical models for the penetration of semi-infinite targets by rigid,deformable and erosive long rods 被引量:18
1
作者 He-Ming Wen Bin Lan 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2010年第4期573-583,共11页
A theoretical study is presented herein on the pen- etration of a semi-infinite target by a spherical-headed long rod for Yp 〉 S, where Yp is the penetrator strength and S is the static target resistance. For Yp 〉 S... A theoretical study is presented herein on the pen- etration of a semi-infinite target by a spherical-headed long rod for Yp 〉 S, where Yp is the penetrator strength and S is the static target resistance. For Yp 〉 S, depending upon initial impact velocity, there exist three types of penetration, namely, penetration by a rigid long rod, penetration by a deforming non-erosive long rod and penetration by an erosive long rod. If the impact velocity of the penetrator is higher than the hydrodynamic velocity (VH), it will penetrate the target in an erosive mode; if the impact velocity lies between the hydrodynamic velocity (VH) and the rigid body velocity (VR), it will penetrate the target in a deformable mode; if the impact velocity is less than the rigid body velocity (VR), it will penetrate the target in a rigid mode. The critical conditions for the transition among these three penetration modes are proposed. It is demonstrated that the present model predictions correlate well with the experimental observations in terms of depth of penetration (DOP) and the critical transition conditions. 展开更多
关键词 Long rod Semi-infinite target - Penetration Alekseevskii-Tate model rigid body velocity - Hydrodynamic velocity
在线阅读 下载PDF
Study of helicopter autorotation landing following engine failure based on a six-degree-of-freedom rigid-body dynamic model 被引量:13
2
作者 Meng Wanli Chen Renliang 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2013年第6期1380-1388,共9页
This paper focuses on the prediction of the safe autorotation landing operations of a helicopter following engine failure.The autorotation landing procedure is formulated as a nonlinear optimal control problem based o... This paper focuses on the prediction of the safe autorotation landing operations of a helicopter following engine failure.The autorotation landing procedure is formulated as a nonlinear optimal control problem based on an augmented six-degree-of-freedom rigid-body flight dynamic model.First,the cost function and constraints are properly selected.The direct transcription approach is then employed to solve the optimal control problem.For a UH-60 helicopter,the optimal solutions with the rigid-body model are compared with those obtained using a two-dimensional point-mass model.It is found that the optimal solutions using the two different models show reasonably good agreement,and furthermore the optimal solutions using the rigid-body model involve the time histories of angular rates and attitudes,lateral velocity and position,as well as pitch controls.Finally the optimal control formulations with different cost functions are proposed for taking account of 1-s time delay and minimum touchdown speed.The calculated control strategies and trajectories are realistic. 展开更多
关键词 Autorotation landing Engine failure Helicopters Optimal control rigid-body model
原文传递
Alternating Parity Band in Octupole-Soft ^(140)Xe with Axial Vibrational-Rotational Model and Triaxial Rigid Rotor Model
3
作者 Xiao Lu Bin Qi Shou-Yu Wang 《Chinese Physics Letters》 SCIE CAS CSCD 2018年第10期9-13,共5页
Energies of the yrast positive-and negative-parity excited states in140 Xe are reproduced by two different models considering quadrupole-octupole deformations, namely the axial vibrational-rotational model and the tri... Energies of the yrast positive-and negative-parity excited states in140 Xe are reproduced by two different models considering quadrupole-octupole deformations, namely the axial vibrational-rotational model and the triaxial rigid rotor model, and compared with the stable octupole-deformed222 Th. The origin of the energy difference between the opposite parity sequences is considered from two different mechanisms, the vibration in axial deformed energy minima and the rotation considering the effective triaxial deformation. The success of reproducing the data in both the models implies that these two mechanisms are equivalent on some level for the octupole-soft nuclei. By investigating the probability distributions for projection of total angular momentum in the triaxial rigid rotor model, it is found that such an energy difference is associated with the difference of orientation of the rotational axis. 展开更多
关键词 Alternating Parity Band in Octupole-Soft Xe with Axial Vibrational-Rotational model and Triaxial rigid Rotor model
原文传递
Kinematic simulation of human gait with a multi-rigid-body foot model 被引量:2
4
作者 YANG Yan HU Xiaochun LI Xiaopeng 《Computer Aided Drafting,Design and Manufacturing》 2012年第2期42-46,共5页
The paper builds a multi-rigid-body model of human with a 4-rigid-body foot in the 3D CAD software Solidworks, based on human anatomy. By controlling the rotation of the ankle and major joints of human body while walk... The paper builds a multi-rigid-body model of human with a 4-rigid-body foot in the 3D CAD software Solidworks, based on human anatomy. By controlling the rotation of the ankle and major joints of human body while walking, the Kinematic simulation was performed in the dynamics simulation software ADAMS. The paper analyzes the simulate results and points out deficiencies in the current work and the direction of research efforts in future. 展开更多
关键词 multi-rigid-body foot model human gait SIMULATION
在线阅读 下载PDF
Dynamic model for landsliding monitoring under rigid body assumption
5
作者 朱建军 丁晓利 陈永奇 《中国有色金属学会会刊:英文版》 CSCD 2001年第2期301-306,共6页
Based on the assumption that the slope bodies are rigid, the dynamic model of the landsiding (forward model) was put forward. According to the dynamic model, the system equations of Kalman filter were constituted. The... Based on the assumption that the slope bodies are rigid, the dynamic model of the landsiding (forward model) was put forward. According to the dynamic model, the system equations of Kalman filter were constituted. The mechanical status of a slope was hence combined with the monitoring data by Kalman filter. The model uncertainties or model errors could also be considered through some fictitious observation equations. Different from existed methods, the presented method can make use for not only the statistic information contained in the data but also the information provided by the mechanical and geological aspect of slopes. At last a numerical example was given out to show the feasibility of the method. [ 展开更多
关键词 dynamic model KALMAN filter rigid body LANDSLIDE MONITORING
在线阅读 下载PDF
Non-rigid 3D models retrieval based on hierarchical matching
6
作者 Liu Yujie Li Wei +3 位作者 Song Yang Gong Weiqing Li Zongmin Li Hua 《Computer Aided Drafting,Design and Manufacturing》 2017年第1期39-47,共9页
In 3D models retrieval, feature description and retrieval of non-rigid model face more complex problems due to the isometry transformation of itself. We introduce the hierarchical combination matching into the feature... In 3D models retrieval, feature description and retrieval of non-rigid model face more complex problems due to the isometry transformation of itself. We introduce the hierarchical combination matching into the feature comparison, and build a map between the divided regions of two models, and then achieve accurate feature matching based on patch-by-patch, which successfully introduces the spatial information into feature matching. Verified by experiment, the 3D model retrieval method proposed in this paper based on hierarchical combination matching can make sure more accurate feature matching, so as to enhance the precision of retrieval. 展开更多
关键词 non-rigid 3D model shape descriptor spatial distribution hierarchical combination matching
在线阅读 下载PDF
A DYNAMIC MODEL FOR ROCKET LAUNCHER WITHCOUPLED RIGID AND FLEXIBLE MOTION
7
作者 章定国 肖建强 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2005年第5期609-617,共9页
The dynamics of a coupled rigid-flexible rocket launcher is reported. The coupled rigid-flexible rocket launcher is divided into two subsystems, one is a system of rigid bodies, the other a flexible launch tube which ... The dynamics of a coupled rigid-flexible rocket launcher is reported. The coupled rigid-flexible rocket launcher is divided into two subsystems, one is a system of rigid bodies, the other a flexible launch tube which can undergo large overall motions spatially. First, the mathematical models for these two subsystems were established respectively. Then the dynamic model for the whole system was obtained by considering the coupling effect between these two subsystems. The approach, which divides a complex system into several simple subsystems first and then obtains the dynamic model for the whole system via combining the existing dynamic models for simple subsystems, can make the modeling procedure efficient and convenient. 展开更多
关键词 coupled rigid-flexible system rocket launcher dynamic modeling
在线阅读 下载PDF
STATISTICAL MODELS FOR SEMI-RIGID NEMATIC POLYMERS
8
作者 王新久 《Chinese Journal of Polymer Science》 SCIE CAS CSCD 1995年第4期361-365,共5页
Semi-rigid liquid crystal polymer is a class of liquid crystal polymers different from long rigid rod liquid crystal polymer to which the well-known Onsager and Flory theories are applied. In this paper, three statist... Semi-rigid liquid crystal polymer is a class of liquid crystal polymers different from long rigid rod liquid crystal polymer to which the well-known Onsager and Flory theories are applied. In this paper, three statistical models for the semi-rigid nematic polymer were addressed. They are the elastically jointed rod model, worm-like chain model, and non-homogeneous chain model. The nematic-isotropic transition temperature was examined. The pseudo-second transition temperature is expressed analytically. Comparisons with the experiments were made and the agreements were found. 展开更多
关键词 semi-rigid nematic polymer statistical model elastically-jointed rods worm-like chain non-homogeneous chain
在线阅读 下载PDF
Reverse Monte Carlo Modeling of the Rigidity Percolation Threshold in Ge<SUB>x</SUB>Se<SUB>1-x</SUB>Glassy Networks
9
作者 Moneeb T. M. Shatnawi 《New Journal of Glass and Ceramics》 2015年第3期31-43,共13页
Based on Maxwell’s constraint counting theory, rigidity percolation in GexSe1-x glasses occurs when the mean coordination number reaches the value of 2.4. This corresponds to Ge0.20Se0.80 glass. At this composition, ... Based on Maxwell’s constraint counting theory, rigidity percolation in GexSe1-x glasses occurs when the mean coordination number reaches the value of 2.4. This corresponds to Ge0.20Se0.80 glass. At this composition, the number of constraints experienced by an atom equals the number of degrees of freedom in three dimensions. Hence, at this composition, the network changes from a floppy phase to a rigid phase, and rigidity starts to percolate. In this work, we use reverse Monte Carlo (RMC) modeling to model the structure of Ge0.20Se0.80 glass by simulating its experimental total atomic pair distribution function (PDF) obtained via high energy synchrotron radiation. A three-dimensional configuration of 2836 atoms was obtained, from which we extracted the partial atomic pair distribution functions associated with Ge-Ge, Ge-Se and Se-Se real space correlations that are hard to extract experimentally from total scattering methods. Bond angle distributions, coordination numbers, mean coordination numbers and the number of floppy modes were also extracted and discussed. More structural insights about network topology at this composition were illustrated. The results indicate that in Ge0.20Se0.80 glass, Ge atoms break up and cross-link the Se chain structure, and form structural units that are four-fold coordinated (the GeSe4 tetrahedra). These tetrahedra form the basic building block and are connected via shared Se atoms or short Se chains. The extent of the intermediate ranged oscillations in real space (as extracted from the width of the first sharp diffraction peak) was found to be around 19.6 ?. The bonding schemes in this glass are consistent with the so-called “8-N” rule and can be interpreted in terms of a chemically ordered network model. 展开更多
关键词 Chalcogenide GLASSES rigidity PERCOLATION Reverse Monte Carlo modeling Atomic Pair Distribution Function (PDF) GexSe1-x GLASSES
暂未订购
不同桥型下飞机着陆跑道桥冲击效应对比研究
10
作者 江辉 李翊萱 +3 位作者 曾聪 张亮 赵星燕 孙耀宗 《振动与冲击》 北大核心 2026年第4期198-209,共12页
选取波音737-800着陆两类多跨长联跑道桥作为研究对象,基于联合仿真技术建立机-桥耦合模型,首先以冲击系数为指标,系统研究不同飞机着陆状态和桥梁结构参数下刚构跑道桥冲击效应,并将其与连续梁跑道桥对比。结果表明:飞机着陆刚构跑道... 选取波音737-800着陆两类多跨长联跑道桥作为研究对象,基于联合仿真技术建立机-桥耦合模型,首先以冲击系数为指标,系统研究不同飞机着陆状态和桥梁结构参数下刚构跑道桥冲击效应,并将其与连续梁跑道桥对比。结果表明:飞机着陆刚构跑道桥和连续梁跑道桥冲击系数随两类参数的变化趋势相近,但前者总体较后者更大,这是由于刚构桥整体刚度更大。从分布区间来看,前者主要分布在0.50~0.80,后者则分布在0.20~0.60。随后,基于正交试验法系统评估了飞机着陆两类跑道桥冲击效应的多参数敏感性排序。研究表明:对于刚构跑道桥,着陆质量的影响最为显著,其次为接地速度和着陆俯仰角;而对于连续梁跑道桥,下沉速度是最主要的影响因素,其次为着陆滚转角和接地速度。 展开更多
关键词 跑道桥 冲击系数 机-桥耦合模型 刚构桥 连续梁桥 敏感性分析
在线阅读 下载PDF
力学模型:从质点到连续介质的演变与启示
11
作者 黄再兴 《力学与实践》 2026年第1期161-165,共5页
本文针对不同力学模型之间的关系在专业课程体系中缺乏全面论述的现状,阐述了从基础质点模型经由质点系、刚体、连续介质一直到多场耦合模型的演变路径,说明了不同模型之间的逻辑关联以及一个“好”力学模型需要满足的条件。这些讨论有... 本文针对不同力学模型之间的关系在专业课程体系中缺乏全面论述的现状,阐述了从基础质点模型经由质点系、刚体、连续介质一直到多场耦合模型的演变路径,说明了不同模型之间的逻辑关联以及一个“好”力学模型需要满足的条件。这些讨论有助于学习者在力学知识体系中既见“树木”,又见“森林”。 展开更多
关键词 力学模型 质点 刚体 连续介质
在线阅读 下载PDF
考虑弱刚度构件的行星齿轮箱刚柔耦合动力学特性研究 被引量:1
12
作者 佘开朗 魏超虎 +3 位作者 曹宏瑞 史江海 杨阳 杜明刚 《振动工程学报》 北大核心 2026年第1期99-108,共10页
针对传统集中参数法和有限元法难以建立复杂行星齿轮箱精确动力学模型以及计算量大的问题,提出一种基于多体动力学的刚柔耦合动力学建模方法。利用有限元子结构缩减理论建立柔性体模型,考虑齿圈和传动轴的柔性以及齿轮时变啮合刚度和传... 针对传统集中参数法和有限元法难以建立复杂行星齿轮箱精确动力学模型以及计算量大的问题,提出一种基于多体动力学的刚柔耦合动力学建模方法。利用有限元子结构缩减理论建立柔性体模型,考虑齿圈和传动轴的柔性以及齿轮时变啮合刚度和传递误差等非线性因素,建立了复杂行星齿轮箱刚柔耦合多体动力学模型。基于仿真结果对比分析了刚柔耦合模型的动力学特性。结果表明,刚柔耦合模型的振动信号幅值相对较大,更有利于分析行星齿轮箱的振动特性;传动轴的柔性变形会导致齿轮的动态传递误差增大;柔性齿圈吸收了部分冲击载荷,从而使行星轮系的齿轮副载荷降低,且载荷的波动程度小于刚体模型,在计算行星轮系齿轮载荷时,考虑齿圈柔性的结果更加贴近真实工况。 展开更多
关键词 行星齿轮箱 弱刚度构件 刚柔耦合建模 振动响应 动态传递误差 啮合载荷
在线阅读 下载PDF
MODELING COMPLIANT NON-PENETRATION CONSTRAINT FOR VP MOTION SIMULATION 被引量:2
13
作者 WangZheng TanJianrong LiuZhenyu JiYangjian 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2005年第2期163-168,共6页
A unilateral non-penetration constraint dynamical simulation model withfriction is constructed based on compliant model for mechanical system VP (virtual prototyping)simulation. This model combines computer graphics w... A unilateral non-penetration constraint dynamical simulation model withfriction is constructed based on compliant model for mechanical system VP (virtual prototyping)simulation. This model combines computer graphics with multi-body system dynamics. It avoidshandling multiplicity of solution, such as cases of no solution, multi-solution brought about byfriction during traditional construction of non-penetration constraint based on rigid model. At thesame time, the realism of VE (virtual environment) is improved in process of simulation.Furthermore, the valid condition of rolling and sliding unilateral contact is constituted based onsingular perturbation and linear complementary theory. Finally, the compliant method is verified byan interaction between a multi-legged robot and VE. 展开更多
关键词 Non-penetration constraint Compliant model rigid model DYNAMICS
在线阅读 下载PDF
燃料非刚体模型开发及其在弥散燃料性能分析中的应用
14
作者 刘亚峰 李峙穆 +1 位作者 丛腾龙 顾汉洋 《原子能科学技术》 北大核心 2026年第2期322-330,共9页
燃料元件在核反应堆服役过程中受到复杂的热-机械耦合作用。FuSPAC刚体模型在高燃耗高功率下难以准确描述燃料芯块的真实力学行为,因此在其基础上,使用有限差分法,建立了一种能够考虑弹塑性变形、蠕变、热膨胀及辐照肿胀等非线性力学FPE... 燃料元件在核反应堆服役过程中受到复杂的热-机械耦合作用。FuSPAC刚体模型在高燃耗高功率下难以准确描述燃料芯块的真实力学行为,因此在其基础上,使用有限差分法,建立了一种能够考虑弹塑性变形、蠕变、热膨胀及辐照肿胀等非线性力学FPESPAC模型,以更准确地刻画燃料芯块的应力-应变演化过程,通过对比其解析解及FuSPAC模拟解,验证了新模型的合理性和先进性。结果表明,新模型能够更精确地预测燃料芯块的变形特征,提高了燃料芯块热-机械行为的计算精度。通过均匀化等效模型,对U_(3)Si_(2)-Al弥散燃料进行热力学性能分析,获得了燃料温度变化以及芯块力学位移情况。未来将结合实验数据对模型进行进一步优化,拓展其在先进燃料体系中的应用。 展开更多
关键词 燃料芯块 非刚体模型 弹塑性力学 弥散燃料
在线阅读 下载PDF
风积沙长短桩复合地基承载性能试验研究
15
作者 严小婷 薛凯喜 +3 位作者 易光胜 朱小伟 司鹏超 胡艳香 《建筑结构》 北大核心 2026年第4期122-129,共8页
为了解决湿陷性黄土易发生土层变形、沉降等问题,通过室内长短桩黄土复合地基模型试验,对比了不同风积沙掺量时长短桩复合地基的承载性能差异,分析了风积沙掺量对长短桩复合地基性能的影响机制。研究结果表明:在长短桩复合地基湿陷与非... 为了解决湿陷性黄土易发生土层变形、沉降等问题,通过室内长短桩黄土复合地基模型试验,对比了不同风积沙掺量时长短桩复合地基的承载性能差异,分析了风积沙掺量对长短桩复合地基性能的影响机制。研究结果表明:在长短桩复合地基湿陷与非湿陷工况下,风积沙掺量50%与风积沙掺量0%的长短桩复合地基在沉降量、桩身轴力和桩土应力等变化趋势基本一致。长短桩复合地基未湿陷工况下,与风积沙掺量0%时相比,风积沙掺量为50%时,长短桩复合地基的沉降量增加了28.05%~38.80%,桩土应力比减小了12.5%~21.2%,长桩桩身轴力相差10.77%~15.73%,短桩桩身轴力相差9.25%~21.06%。长短桩复合地基湿陷工况下,与风积沙掺量0%时相比,风积沙掺量为50%时,长桩桩身轴力相差4.67%~26.45%,短桩桩身轴力相差4.70%~15.15%。风积沙掺量0%和风积沙掺量50%的长短桩复合地基在浸水湿陷后桩顶轴力增加了275%和272%。研究表明,风积沙掺量0%和风积沙掺量50%的两种长短桩复合地基承载特性相近,验证了风积沙作为替代材料的可行性,为风积沙的工程应用提供了参考。 展开更多
关键词 复合地基 风积沙混凝土 刚性长短桩 模型试验 承载性能
在线阅读 下载PDF
“格局引导-刚性约束”双重作用下县域土地利用模拟——以南京市六合区为例
16
作者 陈振 郭杰 +3 位作者 欧名豪 何鸿飞 李发志 鲁帆 《中国土地科学》 北大核心 2026年第1期142-154,共13页
研究目的:构建“格局引导—刚性约束”双重作用下土地利用模拟框架,探索国土空间规划政策对未来土地利用的适应性和可持续性,为国土空间规划实施评估及动态优化、土地利用多目标协同治理提供决策参考。研究方法:以南京市六合区为例,设... 研究目的:构建“格局引导—刚性约束”双重作用下土地利用模拟框架,探索国土空间规划政策对未来土地利用的适应性和可持续性,为国土空间规划实施评估及动态优化、土地利用多目标协同治理提供决策参考。研究方法:以南京市六合区为例,设置国土空间格局引导下不同功能分区的差异化土地需求和地类转换规则,并将各类刚性指标作为约束条件,采用PLUS模型模拟规划目标年土地利用结构布局变化情况。研究结果:(1)相较自然发展情景,规划引导与约束情景下研究区土地利用数量变化趋势整体较为缓和,没有出现建设用地无序扩张、优质耕地与核心生态源地大幅缩减等现象;(2)土地利用布局基本实现耕地向北部田园乡村区集中连片,建设用地向南部城镇发展区及城镇开发边界内集聚布局,“两带两楔”生态区内生态用地结构布局趋于优化;(3)部分街道存在城镇开发边界、生态保护红线等布局与国土空间格局定位不适应的问题,导致土地利用变化影响了该区域经济发展和生态系统稳定性。研究结论:未来应持续强化国土空间发展格局和三条控制线等刚性指标对土地利用的引导与约束作用,并结合地方实际,科学优化城镇开发边界布局,加强对生态廊道等生态要素的保护。 展开更多
关键词 国土空间格局 刚性约束 土地利用模拟 PLUS模型
在线阅读 下载PDF
可伸缩带式输送机刚柔耦合多体动力学建模
17
作者 梅雪峰 伍健 +1 位作者 孙晓霞 李勇 《起重运输机械》 2026年第1期70-75,共6页
可伸缩带式输送机是煤矿井下运输原煤的重要设备,对其进行动力学建模研究十分必要。文中通过计算输送带动态弹性模量、建立输送带离散模型、分析输送带与滚筒及托辊的法向接触力和侧向摩擦力进行刚柔耦合多体动力学模型的建立,并通过对... 可伸缩带式输送机是煤矿井下运输原煤的重要设备,对其进行动力学建模研究十分必要。文中通过计算输送带动态弹性模量、建立输送带离散模型、分析输送带与滚筒及托辊的法向接触力和侧向摩擦力进行刚柔耦合多体动力学模型的建立,并通过对可伸缩带式输送机各部件简化、输送带虚拟传感器布置、输送带连接力计算、接触参数设置等利用RecurDyn软件建立可伸缩带式输送机的多体动力学模型,为可伸缩带式输送机动态特性的分析提供了建模模型及仿真方法。 展开更多
关键词 可伸缩带式输送机 多体动力学分析 RecurDyn软件 刚柔耦合 建模
在线阅读 下载PDF
Model-Based Approach to Investigate the Influences of Different Load States to the Vehicle Dynamics of Light Electric Vehicles
18
作者 Harry Ott René Degen +1 位作者 Mats Leijon Margot Ruschitzka 《Journal of Transportation Technologies》 2021年第2期213-230,共18页
The need to find alternative urban mobility solutions for delivery and transport has led mobility companies to devote enormous resources for research-based solutions to increase vehicle safety. This paper documents a ... The need to find alternative urban mobility solutions for delivery and transport has led mobility companies to devote enormous resources for research-based solutions to increase vehicle safety. This paper documents a virtual approach to investigate the influences of different load states to the vehicle dynamic of light electric vehicle. A model basing on a three-dimensional </span><span style="font-family:""><span style="font-family:Verdana;">multibody system was used, which consists of five bodies. By applying methods of multibody modelling the generalized equations of motion were generated. To </span><span style="font-family:Verdana;">include the behavior within the contact point between road and vehicle a</span><span style="font-family:Verdana;"> simplified tire models was added. The implementation of the equations allowed a first validation of the model via simulations. In a final modeling step the simulation results were interpreted in respect of plausibility. Afterwards, the model was simulated numerically to investigate different load states of the vehicle, by applying constant steering stimuli and variable velocities. In sum, the investigated model approach is useful to identify safety relevant parameters and shows the effects of load states to the vehicle dynamics. Furthermore, it behaves plausibly regarding general vehicle dynamics. These results prove </span><span style="font-family:Verdana;">the general usability of the model for the development controllers and esti</span><span style="font-family:Verdana;">mators in driver assistances systems. 展开更多
关键词 Vehicle Dynamics Multibody System TRICYCLE rigid model Numerical Simulation
在线阅读 下载PDF
刚柔耦合响应下的太阳翼位移场重构方法
19
作者 胡本昂 赖王杰 +2 位作者 黄昌洋 林成辉 张顺琦 《动力学与控制学报》 2026年第1期55-63,共9页
随着大型柔性太阳翼在新一代航天器中的广泛应用,其刚柔耦合动力学特性引发的位移场实时监测需求日益凸显.针对现有位移场重构研究多基于静力学工况且难以适应航天器复杂动力学激励的问题,本文提出一种基于混合坐标法与模态叠加原理的... 随着大型柔性太阳翼在新一代航天器中的广泛应用,其刚柔耦合动力学特性引发的位移场实时监测需求日益凸显.针对现有位移场重构研究多基于静力学工况且难以适应航天器复杂动力学激励的问题,本文提出一种基于混合坐标法与模态叠加原理的动态位移场重构方法.通过分析刚柔耦合航天器动力学模型,结合模态分析方法构建了太阳翼全局位移场高精度重构算法.该方法能够在姿态机动与柔性振动耦合工况下,仅需少量传感数据即可实现动态位移场的实时重构.研究结果表明:本文所提方法能够在动力学激励下实现对太阳翼全局位移场的高精度重构. 展开更多
关键词 刚柔耦合航天器 动力学建模 模态叠加原理 位移场重构
在线阅读 下载PDF
基于内聚力模型的水稳碎石基层劈裂试验模拟
20
作者 王硕 唐正光 王成望 《武汉理工大学学报(交通科学与工程版)》 2026年第1期180-185,共6页
为了深入研究半刚性基层混合料中骨料形状和骨料弹性模量对裂缝产生的影响,引入了内聚力模型,据前人研究成果可知双线性模型更适用于半刚性基层模拟,故使用双线性内聚力模型模拟了半刚性基层混合料劈裂试验过程,比较并分析了试验结果和... 为了深入研究半刚性基层混合料中骨料形状和骨料弹性模量对裂缝产生的影响,引入了内聚力模型,据前人研究成果可知双线性模型更适用于半刚性基层模拟,故使用双线性内聚力模型模拟了半刚性基层混合料劈裂试验过程,比较并分析了试验结果和数值模拟结果,研究了骨料形状和骨料弹性模量对劈裂强度、劈裂破坏时的位移及荷载峰值时裂纹损伤所消耗的能量的影响.结果表明:试验结果和双线性内聚力模型数值模拟结果是吻合的,因此可以用数值模型分析半刚性基层力学响应;不同骨料形状对混合料的劈裂强度产生影响,随着骨料边数的增加,破坏强度提高,劈裂强度最高的圆形骨料相较于劈裂强度最低的正五边形骨料提升6.2%,骨料的棱角性有助于提升混合料的劈裂性能;随着骨料弹性模量的增大,混合料的劈裂强度、破坏时的位移及荷载峰值时裂纹损伤所消耗的能量都呈现先增大后减小的趋势,因此,可以适当提升骨料弹性模量,以提升半刚性基层的抗裂性,然而需注意避免骨料弹性模量过大,建议取值在50~70 GPa,以免因骨料弹性模量过大而导致半刚性基层的力学性能下降,当骨料弹性模量为70 GPa时将使劈裂破坏的位移较位移最小值增长11.8%,对半刚性基层抗裂性能影响较为显著. 展开更多
关键词 道路工程 劈裂性能 内聚力模型 半刚性基层 骨料形状 骨料弹性模量
在线阅读 下载PDF
上一页 1 2 96 下一页 到第
使用帮助 返回顶部