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Analytical models for the penetration of semi-infinite targets by rigid,deformable and erosive long rods 被引量:18
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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
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Study of helicopter autorotation landing following engine failure based on a six-degree-of-freedom rigid-body dynamic model 被引量:13
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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
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Alternating Parity Band in Octupole-Soft ^(140)Xe with Axial Vibrational-Rotational Model and Triaxial Rigid Rotor Model
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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
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Kinematic simulation of human gait with a multi-rigid-body foot model 被引量:2
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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
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Dynamic model for landsliding monitoring under rigid body assumption
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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
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Non-rigid 3D models retrieval based on hierarchical matching
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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
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A DYNAMIC MODEL FOR ROCKET LAUNCHER WITHCOUPLED RIGID AND FLEXIBLE MOTION
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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
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STATISTICAL MODELS FOR SEMI-RIGID NEMATIC POLYMERS
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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
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Reverse Monte Carlo Modeling of the Rigidity Percolation Threshold in Ge<SUB>x</SUB>Se<SUB>1-x</SUB>Glassy Networks
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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
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不同桥型下飞机着陆跑道桥冲击效应对比研究
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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
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基于多岛遗传算法的扭力梁悬架优化设计
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作者 周宇 王长昊 张鹏 《洛阳理工学院学报(自然科学版)》 2026年第1期45-50,共6页
为优化扭力梁悬架动态性能,提出了一种基于多岛遗传算法(Multi-Island Genetic Algorithm,MIGA)的多目标协同优化设计方法。以某款样车的后扭力梁悬架为研究对象,构建了扭力梁悬架刚柔耦合多体动力学模型,同时利用悬架运动学特性与柔性... 为优化扭力梁悬架动态性能,提出了一种基于多岛遗传算法(Multi-Island Genetic Algorithm,MIGA)的多目标协同优化设计方法。以某款样车的后扭力梁悬架为研究对象,构建了扭力梁悬架刚柔耦合多体动力学模型,同时利用悬架运动学特性与柔性特性(Kinematic&Compliance,K&C)试验测试修正该模型,并在此基础上,对该模型开展典型K&C工况仿真分析;基于多岛遗传算法构建目标函数权重分配模型,引入岛屿迁移策略及动态收敛判据,实现了在高维解空间中对全局最优解的快速搜索。结果表明:优化后的悬架在纵向位移及侧倾中心高度等关键指标上均表现出更佳的动态响应特性,为扭力梁悬架系统的优化设计提供了可靠的理论基础和工程应用方法。 展开更多
关键词 多岛遗传算法 扭力梁悬架 刚柔耦合模型 动态响应特性
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力学模型:从质点到连续介质的演变与启示
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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
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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
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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
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MODELING COMPLIANT NON-PENETRATION CONSTRAINT FOR VP MOTION SIMULATION 被引量:2
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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
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燃料非刚体模型开发及其在弥散燃料性能分析中的应用
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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
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刚柔复合驱动并联式拣矸机器人动力学与鲁棒模型预测控制
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作者 刘鹏 王毅 +4 位作者 马宏伟 段学超 曹现刚 夏晶 聂珍 《煤炭科学技术》 北大核心 2026年第3期320-334,共15页
矸石分拣可以提升煤炭品质、降低运输成本、减少环境污染,实现煤炭资源的高效清洁利用与矿山可持续发展。传统煤矸石人工分拣存在劳动强度大、效率低的问题,提出刚柔复合驱动并联式拣矸机器人构型方案。但是由于拣矸置矸过程所导致的动... 矸石分拣可以提升煤炭品质、降低运输成本、减少环境污染,实现煤炭资源的高效清洁利用与矿山可持续发展。传统煤矸石人工分拣存在劳动强度大、效率低的问题,提出刚柔复合驱动并联式拣矸机器人构型方案。但是由于拣矸置矸过程所导致的动态冲击和动力学参数的不确定,以及外界干扰等因素,势必会影响拣矸机器人末端抓斗的跟踪精度和稳定性,甚至导致拣矸任务无法完成。鉴于此,开展了刚柔复合驱动并联式拣矸机器人动力学与鲁棒模型预测控制研究。首先,提出了刚柔复合驱动并联式拣矸机器人系统方案,分析了机器人末端抓斗的自由度,并采用矢量封闭原理建立了拣矸机器人的运动学模型。其次,考虑机器人模型参数摄动和拣矸置矸过程的外部扰动,基于牛顿-欧拉方程建立了刚柔复合驱动并联式拣矸机器人的动力学模型。再次,提出了融合张力约束的鲁棒模型预测控制方法,实时优化柔索-推杆驱动力协同分配,动态抵消矸石抓取与置放过程的冲击与外部扰动,实现拣矸机器人末端抓斗高精度轨迹跟踪控制。最后,采用空间螺旋轨迹和4段式分拣轨迹(启动段—准备段—抓矸段—置矸段)对刚柔复合驱动并联式拣矸机器人鲁棒模型预测控制系统进行了仿真分析,结果表明:末端抓斗轨迹最大偏移量仅3.7×10^(-3) m,姿态角误差稳定于3.2×10^(-3) rad,且柔索张力始终满足驱动力约束条件,验证了控制策略对复杂工况下拣矸作业的有效性。 展开更多
关键词 刚柔复合驱动 并联机器人 矸石分拣 鲁棒模型预测控制 鲁棒性
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空间扑翼机构运动学建模、优化及仿真
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作者 许远康 侯悦民 刘磊 《机械设计与制造》 北大核心 2026年第4期328-337,共10页
基于对海鸥飞行照片的图像处理通过测量得到海鸥正常飞行时翅膀的运动参数。依据鸟类尺度效应经验公式和海鸥的骨骼尺寸的相关文献,提出了一种新型空间仿生扑翼机构。以最大扑动角为目标函数,极位夹角及最小传动角的取值范围为约束条件... 基于对海鸥飞行照片的图像处理通过测量得到海鸥正常飞行时翅膀的运动参数。依据鸟类尺度效应经验公式和海鸥的骨骼尺寸的相关文献,提出了一种新型空间仿生扑翼机构。以最大扑动角为目标函数,极位夹角及最小传动角的取值范围为约束条件建立优化模型。基于序列二次规划(SQP)算法对模型进行优化求解得到驱动机构的杆长参数,并通过ADAMS对驱动机构进行运动仿真,通过对比仿真结果中的极位夹角、扑动角、最小传动角的数值,验证了优化结果的准确性。建立空间扑翼机构多刚体运动动力学模型,经余弦相似度计算基于MATLAB机构运动仿真的结果与测量的海鸥飞行时翅膀的运动参数基本一致。 展开更多
关键词 图像处理 空间仿生扑翼机构 机构优化仿真 多体运动学模型 余弦相似度
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风积沙长短桩复合地基承载性能试验研究
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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
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“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
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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
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汽车起重机伸缩臂回缩的动态特性仿真研究
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作者 安书剑 王欣 +1 位作者 刘建强 陈韬羽 《机械设计与制造工程》 2026年第3期11-16,共6页
以25吨级汽车起重机伸缩臂为研究对象,利用ANSYS建立伸缩臂的有限元模型,并将其导入ADAMS中构建整机的刚柔耦合模型。通过动力学仿真,获取了不同回缩缓冲时间下臂头撞块、变幅油缸及底节臂焊缝等关键部位的应力变化曲线。仿真结果表明,... 以25吨级汽车起重机伸缩臂为研究对象,利用ANSYS建立伸缩臂的有限元模型,并将其导入ADAMS中构建整机的刚柔耦合模型。通过动力学仿真,获取了不同回缩缓冲时间下臂头撞块、变幅油缸及底节臂焊缝等关键部位的应力变化曲线。仿真结果表明,随着回落减速时间从0.05 s延长至10.00 s,碰撞后的应力峰值相较于碰撞前稳定值的超出幅度显著降低。 展开更多
关键词 汽车起重机 伸缩臂 刚柔耦合模型 回缩缓冲
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