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高超声速飞行器受热壁板的气动弹性声振分析 被引量:12
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作者 杨智春 刘丽媛 王晓晨 《航空学报》 EI CAS CSCD 北大核心 2016年第12期3578-3587,共10页
高超声速飞行器壁板在非定常气动力、热载荷和噪声载荷构成的多物理场联合作用下,将表现出复杂的非线性气动弹性声振响应,特别是在颤振临界动压附近,受热载荷以及声载荷作用,壁板表现出复杂的跳变运动。基于von Karman大变形板理论,建... 高超声速飞行器壁板在非定常气动力、热载荷和噪声载荷构成的多物理场联合作用下,将表现出复杂的非线性气动弹性声振响应,特别是在颤振临界动压附近,受热载荷以及声载荷作用,壁板表现出复杂的跳变运动。基于von Karman大变形板理论,建立了热-声载荷和气动力共同作用下的壁板运动方程,分析了超声速气流中受热壁板的屈曲变形及热屈曲稳定性,借助势阱概念初步分析了壁板跳变运动产生的机理。通过定义"穿零频次"给出了跳变运动定量的分类方法,并计算得到不同温升和动压情况下,壁板发生跳变运动所对应的临界声压级。结果表明:在颤振临界动压之前,随着动压的增加,受热壁板势阱的深度先增大后减小,且受热壁板的势阱深度随着温升的增加而增大。 展开更多
关键词 壁板 气动弹性 气动加热 声振响应 跳变 热屈曲 势阱
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In-plane elastic stability of fixed parabolic shallow arches 被引量:8
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作者 CAI JianGuo FENG Jian +1 位作者 CHEN Yao HUANG LiFeng 《Science China(Technological Sciences)》 SCIE EI CAS 2009年第3期596-602,共7页
The nonlinear behavior of fixed parabolic shallow arches subjected to a vertical uniform load is inves- tigated to evaluate the in-plane buckling load. The virtual work principle method is used to establish the non-li... The nonlinear behavior of fixed parabolic shallow arches subjected to a vertical uniform load is inves- tigated to evaluate the in-plane buckling load. The virtual work principle method is used to establish the non-linear equilibrium and buckling equations. Analytical solutions for the non-linear in-plane sym- metric snap-through and antisymmetric bifurcation buckling loads are obtained. Based on the least square method, an approximation for the symmetric buckling load of fixed parabolic arch is proposed to simplify the solution process. And the relation between modified slenderness and buckling modes are discussed. Comparisons with the results of finite element analysis demonstrate that the solutions are accurate. A cable-arch structure is presented to improve the in-plane stability of parabolic arches. The comparison of buckling loads between cable-arch systems and arches only show that the effect of cables becomes more evident with the increase of arch’s modified slenderness. 展开更多
关键词 PARABOLIC ARCH elastic stability SHALLOW BIFURCATION snap-through
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An Oscillating Wave Energy Converter with Nonlinear Snap-Through Power-Take-Off Systems in Regular Waves 被引量:7
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作者 张显涛 杨建民 肖龙飞 《China Ocean Engineering》 SCIE EI CSCD 2016年第4期565-580,共16页
Floating oscillating bodies constitute a large class of wave energy converters, especially for offshore deployment. Usually the Power-Take-Off(PTO) system is a directly linear electric generator or a hydraulic motor... Floating oscillating bodies constitute a large class of wave energy converters, especially for offshore deployment. Usually the Power-Take-Off(PTO) system is a directly linear electric generator or a hydraulic motor that drives an electric generator. The PTO system is simplified as a linear spring and a linear damper. However the conversion is less powerful with wave periods off resonance. Thus, a nonlinear snap-through mechanism with two symmetrically oblique springs and a linear damper is applied in the PTO system. The nonlinear snap-through mechanism is characteristics of negative stiffness and double-well potential. An important nonlinear parameter γ is defined as the ratio of half of the horizontal distance between the two springs to the original length of both springs. Time domain method is applied to the dynamics of wave energy converter in regular waves. And the state space model is used to replace the convolution terms in the time domain equation. The results show that the energy harvested by the nonlinear PTO system is larger than that by linear system for low frequency input. While the power captured by nonlinear converters is slightly smaller than that by linear converters for high frequency input. The wave amplitude, damping coefficient of PTO systems and the nonlinear parameter γ affect power capture performance of nonlinear converters. The oscillation of nonlinear wave energy converters may be local or periodically inter well for certain values of the incident wave frequency and the nonlinear parameter γ, which is different from linear converters characteristics of sinusoidal response in regular waves. 展开更多
关键词 wave energy power-take-off snap-through time domain equation state space dynamic response
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Nonlinear energy harvesting based on a modified snap-through mechanism 被引量:7
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作者 Zeqi LU Ke LI +1 位作者 Hu DING Liqun CHEN 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2019年第1期167-180,共14页
A modified snap-through mechanism is used in an electromagnetic energy harvester to improve its effectiveness. It mainly comprises three springs that are configured so that the potential energy of the system has two s... A modified snap-through mechanism is used in an electromagnetic energy harvester to improve its effectiveness. It mainly comprises three springs that are configured so that the potential energy of the system has two stable equilibrium points. In particular, the small vibration behavior of the harvester around one of the equilibriums is of interest. A multi-scale method(MSM) is used to analyze the frequency response curve. Two snap-through mechanisms are considered. One has both horizontal and vertical springs. The other has only horizontal springs. The frequency response curves of these two classes are compared under the same excitation and electric loading conditions. The latter exhibits more bending of the frequency response curve than the former one. The results are also validated by some numerical work. The averaged power subject to the Gaussian white noise is calculated numerically, and the results demonstrate that bi-stable energy harvesting with only horizontal springs can outperform the mechanism with both horizontal and vertical springs for the same distance between two equilibriums. 展开更多
关键词 energy HARVESTING NONLINEAR STIFFNESS snap-through RANDOM EXCITATION
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Arc-length technique for nonlinear finite element analysis 被引量:9
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作者 MEMONBashir-Ahmed 苏小卒 《Journal of Zhejiang University Science》 EI CSCD 2004年第5期618-628,共11页
Nonlinear solution of reinforced concrete structures, particularly complete load-deflection response, requires tracing of the equilibrium path and proper treatment of the limit and bifurcation points. In this regard, ... Nonlinear solution of reinforced concrete structures, particularly complete load-deflection response, requires tracing of the equilibrium path and proper treatment of the limit and bifurcation points. In this regard, ordinary solution techniques lead to instability near the limit points and also have problems in case of snap-through and snap-back. Thus they fail to predict the complete load-displacement response. The arc-length method serves the purpose well in principle, received wide acceptance in finite element analysis, and has been used extensively. However modifications to the basic idea are vital to meet the particular needs of the analysis. This paper reviews some of the recent developments of the method in the last two decades, with particular emphasis on nonlinear finite element analysis of reinforced concrete structures. 展开更多
关键词 Arc-length method Nonlinear analysis Finite element method Reinforced concrete Load-deflection path Document code: A CLC number: TU31 Arc-length technique for nonlinear finite element analysis* MEMON Bashir-Ahmed# SU Xiao-zu (苏小卒) (Department of Structural Engineering Tongji University Shanghai 200092 China) E-mail: bashirmemon@sohu.com xiaozub@online.sh.cn Received July 30 2003 revision accepted Sept. 11 2003 Abstract: Nonlinear solution of reinforced concrete structures particularly complete load-deflection response requires tracing of the equilibrium path and proper treatment of the limit and bifurcation points. In this regard ordinary solution techniques lead to instability near the limit points and also have problems in case of snap-through and snap-back. Thus they fail to predict the complete load-displacement response. The arc-length method serves the purpose well in principle received wide acceptance in finite element analysis and has been used extensively. However modifications to the basic idea are vital to meet the particular needs of the analysis. This paper reviews some of the recent developments of the method in the last two decades with particular emphasis on nonlinear finite element analysis of reinforced concrete structures. Key words: Arc-length method Nonlinear analysis Finite element method Reinforced concrete Load-deflection path
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热声载荷下薄壁结构振动响应试验验证与疲劳分析 被引量:7
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作者 沙云东 王建 +1 位作者 赵奉同 骆丽 《航空动力学报》 EI CAS CSCD 北大核心 2017年第11期2659-2671,共13页
由于热声环境下金属薄壁结构表现出复杂的大挠度强非线性振动响应特性,影响结构的疲劳性能与寿命,结合有限元法与降阶模态法对四边固支高温合金矩形薄壁结构的热声响应进行计算。结果研究发现:屈曲后结构出现跳变运动且应力循环呈三角... 由于热声环境下金属薄壁结构表现出复杂的大挠度强非线性振动响应特性,影响结构的疲劳性能与寿命,结合有限元法与降阶模态法对四边固支高温合金矩形薄壁结构的热声响应进行计算。结果研究发现:屈曲后结构出现跳变运动且应力循环呈三角状分布,热声载荷的相对强弱决定了跳变形式。采用改进雨流计数法、Morrow平均应力模型、Miner线性损伤累积理论计算热声疲劳寿命,屈曲前到临界屈曲时应力循环损伤量级显著增大,由10-5增大到10-4,寿命随温度增加呈先减小后增加趋势。开展薄壁结构热声试验,并将仿真计算结果与试验结果进行对比,结果表明结构的模态频率偏差不超过1Hz,动态应变响应结果的量值相当,验证了薄壁结构热声响应计算方法与模型的有效性。 展开更多
关键词 热声载荷 非线性振动响应 疲劳寿命 屈曲 跳变 试验验证
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Tuning of Multi-stability Profile and Transition Sequence of Stacked Miura-Origami Metamaterials 被引量:2
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作者 Haiping Wu Hongbin Fang 《Acta Mechanica Solida Sinica》 SCIE EI CSCD 2023年第4期554-568,共15页
Multi-stable origami structures and metamaterials possess unique advantages and could exhibit multiple stable three-dimensional configurations,which have attracted widespread research interest and held promise for app... Multi-stable origami structures and metamaterials possess unique advantages and could exhibit multiple stable three-dimensional configurations,which have attracted widespread research interest and held promise for applications in many fields.Although a great deal of attention has been paid to the design and application of multi-stable origami structures,less knowledge is available about the transition sequence among different stable configurations,especially in terms of the fundamental mechanism and the tuning method.To fill this gap,with the multi-stable dual-cell stacked Miura-ori chain as a platform,this paper explores the rules that govern the configuration transition and proposes effective methods for tuning the transition sequence.Specifically,by correlating the energy evolution,the transition paths,and the associated force-displace-ment profiles,we find that the critical extension/compression forces of the component cells play a critical role in governing the transition sequence.Accordingly,we summarize the rules for predicting the transition sequence:the component cell that first reaches the critical force during quasi-static extension or compression will be the first to undergo a configuration switch.Based on these findings,two methods,i.e.,a design method based on crease-stiffness assignment and an online method based on internal pressure regulation,are proposed to tune the stability profile and the transition sequence of the multi-stable origami structure.The crease-stiffness design approach,although effective,cannot be employed for online tuning once the prototype has been fabricated.The pressure-based approach,on the other hand,has been shown experimentally to be effective in adjusting the constitutive force-displacement profiles of the component cells and,in turn,tuning the transition sequence according to the summarized rules.The results of this study will advance the state of the art of origami mechanics and promote the engineering applications of multi-stable origami metamaterials. 展开更多
关键词 Origami metamaterial Bi-stability Origami mechanics Pneumatic origami snap-through transition
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Numerical evaluation of buckling behavior in space structure considering geometrical parameters with joint rigidity 被引量:6
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作者 Su-Deok Shon Kyung-Ju Hwang Seung-Jae Lee 《Journal of Central South University》 SCIE EI CAS 2014年第3期1115-1124,共10页
The buckling behavior of single layer space structure is very sensitive. The joint rigidity, moreover, is one of the main factors of stability which may determine the entire failure behavior. Thus, the reasonable stif... The buckling behavior of single layer space structure is very sensitive. The joint rigidity, moreover, is one of the main factors of stability which may determine the entire failure behavior. Thus, the reasonable stiffness of joint system, which is neither total pin assumption nor perfect fix condition, is very important to apply to the real single layer space one. Therefore, the purpose of this work was to investigate the buckling behavior of single layer space structure, using the development of the upgraded stiffness matrix for the joint rigidity. To derive tangential stiffness matrix, a displacement function was assumed using translational and rotational displacement at the node. The geometrical nonlinear analysis was simulated not only with perfect model but also with imperfect one. As a result, the one and two free nodal numerical models were investigated using derived stiffness matrix. It was figured out that the buckling load increases in proportion to joint rigidity with rise-span ratio. The stability of numerical model is very sensitive with the initial imperfection, responding of bifurcation in the structure. 展开更多
关键词 space frame geometric nonlinearity snap-through BIFURCATION initial imperfection joint rigidity
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热冲击下四边简支浅壳的动态突跳行为
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作者 孙伟 何利文 《应用力学学报》 CAS CSCD 北大核心 2024年第3期621-628,共8页
准确地分析和预测浅壳结构在热冲击下的动态稳定性和结构完整性,对于工程中普遍使用的壳结构的设计和优化具有重要意义。利用非线性浅壳理论,并使用Ritz法和Newmark直接积分法研究了内表面受热冲击作用的四边简支各向同性浅壳的动态突跳... 准确地分析和预测浅壳结构在热冲击下的动态稳定性和结构完整性,对于工程中普遍使用的壳结构的设计和优化具有重要意义。利用非线性浅壳理论,并使用Ritz法和Newmark直接积分法研究了内表面受热冲击作用的四边简支各向同性浅壳的动态突跳(snap-through)行为。分析结果表明:浅壳在足够强的热冲击下会发生动态突跳,而在突跳前后都会发生较剧烈的热振动;Budiansky-Hutchinson准则可用于判定发生动态突跳的临界热冲击条件。 展开更多
关键词 热冲击 浅壳 突跳 Budiansky-Hutchinson准则
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Giant Flexoelectric Effect in Snapping Surfaces Enhanced by Graded Stiffness
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作者 Chuo Zhao 《Acta Mechanica Solida Sinica》 SCIE EI CSCD 2024年第4期528-540,共13页
Flexoelectricity is present in nonuniformly deformed dielectric materials and has size-dependent properties, making it useful for microelectromechanical systems. Flexoelectricity is small compared to piezoelectricity;... Flexoelectricity is present in nonuniformly deformed dielectric materials and has size-dependent properties, making it useful for microelectromechanical systems. Flexoelectricity is small compared to piezoelectricity;therefore, producing a large-scale flexoelectric effect is of great interest. In this paper, we explore a way to enhance the flexoelectric effect by utilizing the snap-through instability and a stiffness gradient present along the length of a curved dielectric plate. To analyze the effect of stiffness profiles on the plate, we employ numerical parameter continuation. Our analysis reveals a nonlinear relationship between the effective electromechanical coupling coefficient and the gradient of Young’s modulus. Moreover, we demonstrate that the quadratic profile is more advantageous than the linear profile. For a dielectric plate with a quadratic profile and a modulus gradient of − 0.9, the effective coefficient can reach as high as 15.74 pC/N, which is over three times the conventional coupling coefficient of piezoelectric material. This paper contributes to our understanding of the amplification of flexoelectric effects by harnessing snapping surfaces and stiffness gradient design. 展开更多
关键词 Functionally graded material FLEXOELECTRICITY Numerical continuation snap-through instability
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Snap-through behaviors and nonlinear vibrations of a bistable composite laminated cantilever shell:an experimental and numerical study
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作者 Lele REN Wei ZHANG +1 位作者 Ting DONG Yufei ZHANG 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2024年第5期779-794,共16页
The snap-through behaviors and nonlinear vibrations are investigated for a bistable composite laminated cantilever shell subjected to transversal foundation excitation based on experimental and theoretical approaches.... The snap-through behaviors and nonlinear vibrations are investigated for a bistable composite laminated cantilever shell subjected to transversal foundation excitation based on experimental and theoretical approaches.An improved experimental specimen is designed in order to satisfy the cantilever support boundary condition,which is composed of an asymmetric region and a symmetric region.The symmetric region of the experimental specimen is entirely clamped,which is rigidly connected to an electromagnetic shaker,while the asymmetric region remains free of constraint.Different motion paths are realized for the bistable cantilever shell by changing the input signal levels of the electromagnetic shaker,and the displacement responses of the shell are collected by the laser displacement sensors.The numerical simulation is conducted based on the established theoretical model of the bistable composite laminated cantilever shell,and an off-axis three-dimensional dynamic snap-through domain is obtained.The numerical solutions are in good agreement with the experimental results.The nonlinear stiffness characteristics,dynamic snap-through domain,and chaos and bifurcation behaviors of the shell are quantitatively analyzed.Due to the asymmetry of the boundary condition and the shell,the upper stable-state of the shell exhibits an obvious soft spring stiffness characteristic,and the lower stable-state shows a linear stiffness characteristic of the shell. 展开更多
关键词 bistable composite laminated cantilever shell snap-through behavior nonlinear vibration nonlinear stiffness characteristic chaos and bifurcation
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Inter-well internal resonance analysis of rectangular asymmetric cross-ply bistable composite laminated cantilever shell under transverse foundation excitation
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作者 Lele REN Wei ZHANG Yufei ZHANG 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2024年第8期1353-1370,共18页
The chaotic dynamic snap-through and complex nonlinear vibrations are investigated in a rectangular asymmetric cross-ply bistable composite laminated cantilever shell,in cases of 1:2 inter-well internal resonance and ... The chaotic dynamic snap-through and complex nonlinear vibrations are investigated in a rectangular asymmetric cross-ply bistable composite laminated cantilever shell,in cases of 1:2 inter-well internal resonance and primary resonance.The transverse foundation excitation is applied to the fixed end of the structure,and the other end is in a free state.The first-order approximate multiple scales method is employed to perform the perturbation analysis on the dimensionless two-degree-of-freedom ordinary differential motion control equation.The four-dimensional averaged equations are derived in both polar and rectangular coordinate forms.Deriving from the obtained frequency-amplitude and force-amplitude response curves,a detailed analysis is conducted to examine the impacts of excitation amplitude,damping coefficient,and tuning parameter on the nonlinear internal resonance characteristics of the system.The nonlinear softening characteristic is exhibited in the upper stable-state,while the lower stable-state demonstrates the softening and linearity characteristics.Numerical simulation is carried out using the fourth-order Runge-Kutta method,and a series of nonlinear response curves are plotted.Increasing the excitation amplitude further elucidates the global bifurcation and chaotic dynamic snap-through characteristics of the bistable cantilever shell. 展开更多
关键词 bistable composite laminated cantilever shell inter-well internal resonance primary resonance chaotic dynamic snap-through complex nonlinear vibration
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Theoretical and experimental investigation of the resonance responses and chaotic dynamics of a bistable laminated composite shell in the dynamic snap-through mode
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作者 Meiqi WU Pengyu LV +3 位作者 Hongyuan LI Jiale YAN Huiling DUAN Wei ZHANG 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2024年第4期581-602,共22页
The dynamic model of a bistable laminated composite shell simply supported by four corners is further developed to investigate the resonance responses and chaotic behaviors.The existence of the 1:1 resonance relations... The dynamic model of a bistable laminated composite shell simply supported by four corners is further developed to investigate the resonance responses and chaotic behaviors.The existence of the 1:1 resonance relationship between two order vibration modes of the system is verified.The resonance response of this class of bistable structures in the dynamic snap-through mode is investigated,and the four-dimensional(4D)nonlinear modulation equations are derived based on the 1:1 internal resonance relationship by means of the multiple scales method.The Hopf bifurcation and instability interval of the amplitude frequency and force amplitude curves are analyzed.The discussion focuses on investigating the effects of key parameters,e.g.,excitation amplitude,damping coefficient,and detuning parameters,on the resonance responses.The numerical simulations show that the foundation excitation and the degree of coupling between the vibration modes exert a substantial effect on the chaotic dynamics of the system.Furthermore,the significant motions under particular excitation conditions are visualized by bifurcation diagrams,time histories,phase portraits,three-dimensional(3D)phase portraits,and Poincare maps.Finally,the vibration experiment is carried out to study the amplitude frequency responses and bifurcation characteristics for the bistable laminated composite shell,yielding results that are qualitatively consistent with the theoretical results. 展开更多
关键词 bistable laminated composite shell dynamic snap-through mode Hopf bifurcation chaotic dynamics vibration experiment
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Static and dynamic snap-through behaviour of an elastic spherical shell 被引量:3
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作者 D. Karagiozova X.-W. Zhang T.-X. Yu 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2012年第3期695-710,共16页
The deformation and snap-through behaviour of a thin-walled elastic spherical shell statically compressed on a flat surface or impacted against a fiat surface are studied the- oretically and numerically in order to es... The deformation and snap-through behaviour of a thin-walled elastic spherical shell statically compressed on a flat surface or impacted against a fiat surface are studied the- oretically and numerically in order to estimate the influence of the dynamic effects on the response. A table tennis ball is considered as an example of a thin-walled elastic shell. It is shown that the increase of the impact velocity leads to a variation of the deformed shape thus resulting in larger de- formation energy. The increase of the contact force is caused by both the increased contribution of the inertia forces and contribution of the increased deformation energy. The contact force resulted from deformation/inertia of the ball and the shape of the deformed region are calcu- lated by the proposed theoretical models and compared with the results from both the finite element analysis and some previously obtained experimental data. Good agreement is demonstrated. 展开更多
关键词 Elastic spherical shell snap-through buckling.Static Dynamic
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Probability-Based Analyses of the Snap-Through in Cage-Shaped Mesostructures Under Out-of-Plane Compressions 被引量:1
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作者 Qing Liu Zhangming Shen +5 位作者 Zhi Liu Yumeng Shuai Zengyao Lv Tianqi Jin Xu Cheng Yihui Zhang 《Acta Mechanica Solida Sinica》 SCIE EI CSCD 2023年第4期569-581,共13页
Three-dimensional(3D)mesostructures with distinct compressive deformation behaviors and tunable mechanical responses have gained increasing interest in recent years.3D cage-shaped mesostructures are representative fra... Three-dimensional(3D)mesostructures with distinct compressive deformation behaviors and tunable mechanical responses have gained increasing interest in recent years.3D cage-shaped mesostructures are representative framework structures widely exploited in 3D flexible electronics,owing to their unique cellular geometry and unusual mechanical responses.The snap-through behavior of cage-shaped mesostructures could potentially result in the performance degradation of electronics,while it could also be harnessed to design reconfigurable electronics.Due to the complicated deformation modes and random characteristics in experiments,the snap-through behavior of cage-shaped mesostructures remains largely unexplored,espe-cially in terms of probability-based analyses.In this work,we present a systematic study on the configuration evolution and snap-through of 3D cage-shaped mesostructures under out-of-plane compressions.Experimental and computational studies show the existence of two distinct deformation modes associated with the snap-through,which is controlled by the energy barrier based on the energetic analyses.Phase diagrams of the deformation modes decode how key geometric parameters and assembly strain affect the snap-through.Compressive experiments based on periodic arrays(10 × 10)of mesostructures provided a large amount of deformation data,allowing for statistical analyses of the snap-through behavior.These results provide new insights and useful guidelines for the design of 3D reconfigurable devices and multistable metamaterials based on 3D cage-shaped mesostructures. 展开更多
关键词 3D cage-shaped mesostructures snap-through Probability-based analyses 3D assembly Out-of-plane compression
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Analytical modeling for rapid design of bistable buckled beams 被引量:2
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作者 Wenzhong Yan Yunchen Yu Ankur Mehta 《Theoretical & Applied Mechanics Letters》 CAS CSCD 2019年第4期264-272,I0003,共10页
Double-clamped bistable buckled beams demonstrate great versatility in various fields such as robotics,energy harvesting,and microelectromechanical system(MEMS).However,their design often requires time-consuming and e... Double-clamped bistable buckled beams demonstrate great versatility in various fields such as robotics,energy harvesting,and microelectromechanical system(MEMS).However,their design often requires time-consuming and expensive computations.In this work,we present a method to easily and rapidly design bistable buckled beams subjected to a transverse point force.Based on the Euler–Bernoulli beam theory,we establish a theoretical model of bistable buckled beams to characterize their snapthrough properties.This model is verified against the results from a finite element analysis(FEA)model,with maximum discrepancy less than 7%.By analyzing and simplifying our theoretical model,we derive explicit analytical expressions for critical behavioral values on the force-displacement curve of the beam.These behavioral values include critical force,critical displacement,and travel,which are generally sufficient for characterizing the snapthrough properties of a bistable buckled beam.Based on these analytical formulas,we investigate the influence of a bistable buckled beam's key design parameters,including its actuation position and precompression,on its critical behavioral values,with our results validated by FEA simulations.Our analytical method enables fast and computationally inexpensive design of bistable buckled beams and can guide the design of complicated systems that incorporate bistable mechanisms. 展开更多
关键词 BISTABLE buckled beam THEORETICAL model snap-through characteristics Off-center ACTUATION Analytical expression Rapid design
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Characteristics of bifurcation and buckling load of space truss in consideration of initial imperfection and load mode 被引量:2
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作者 Su-deok SHON Seung-jae LEE Kang-guk LEE 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2013年第3期206-218,共13页
This study investigated characteristics of bifurcation and critical buckling load by shape imperfection of space truss,which were sensitive to initial conditions.The critical point and buckling load were computed by t... This study investigated characteristics of bifurcation and critical buckling load by shape imperfection of space truss,which were sensitive to initial conditions.The critical point and buckling load were computed by the analysis of the eigenvalues and determinants of the tangential stiffness matrix.The two-free-nodes example and star dome were selected for the case study in order to examine the nodal buckling and global buckling by the sensitivity to the eigen buckling mode and the analyses of the influence,and characteristics of the parameters as defined by the load ratio of the center node and surrounding node,as well as rise-span ratio were performed.The sensitivity to the imperfection of the initial shape of the two-free-nodes example,which occurs due to snapping at the critical point,resulted in bifurcation before the limit point due to the buckling mode,and the buckling load was reduced by the increase in the amount of imperfection.The two sensitive buckling patterns of the numerical model are established by investigating the displaced position of the free nodes,and the asymmetric eigenmode greatly influenced the behavior of the imperfection shape whether it was at limit point or bifurcation.Furthermore,the sensitive mode of the two-free-nodes example was similar to the in-extensional basis mechanism of a simplified model.The star dome,which was used to examine the influence among several nodes,indicated that the influence of nodal buckling was greater than that of global buckling as the rise-span ratio was higher.Besides,global buckling is occurred with reaching bifurcation point as the value of load ratio was higher,and the buckling load level was about 50%-70% of load level at limit point. 展开更多
关键词 Space truss Geometric nonlinearity Initial imperfection snap-through BIFURCATION Global buckling
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Theoretical study of the electroactive bistable actuator and regulation methods
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作者 Wenjie Sun Huwei Liang +1 位作者 Fei Zhang Bo Li 《International Journal of Smart and Nano Materials》 SCIE EI 2023年第1期36-56,共21页
Dielectric elastomer actuators have attracted growing interest for soft robot due to their large deformation and fast response.However,continuous high-voltage loading tends to cause the electric breakdown of the actua... Dielectric elastomer actuators have attracted growing interest for soft robot due to their large deformation and fast response.However,continuous high-voltage loading tends to cause the electric breakdown of the actuator due to heat accumulation,and viscoelasticity complicates precise control.The snap-through bistability of the Venus flytrap is one of the essential inspirations for bionic structure,which can be adopted to improve the shortcoming of dielectric elastomer actuators and develop a new actuation structure with low energy consumption,variable configuration,and multi-mode actuation.Hence,in this paper,the structural design principles of electroactive bistable actuators are first presented based on the total potential energy of the structure.Following that,a feasible design parameter region is provided,the influence of crucial parameters on the actuation stroke,trigger voltage,and actuation charge are discussed.Finally,according to the coupling relationship between the bending stiffness and the bistable property of the actuator,the adjusting methods of bistable actuation are explored.A qualitative experiment was performed to verify the feasibility and correctness of the bistable design methodology and the actuation regulation strategy.This study provides significant theoretical guidance and technical support for developing and applying dielectric elastomer actuators with multi-mode,high-performance,and long-life characteristics. 展开更多
关键词 Dielectric elastomer bistable structure snap-through electromechanical actuation minimum energy structure
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反对称铺层碳纤维复合材料圆柱壳的双稳态应力特性 被引量:4
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作者 张淑杰 李国泽 +1 位作者 周阳 沈海军 《国防科技大学学报》 EI CAS CSCD 北大核心 2021年第3期32-37,共6页
双稳态复合材料可广泛应用于各类可变结构的设计。针对反对称铺层的圆柱壳,利用有限元软件ABAQUS的Standard准静态分析,模拟其双稳态跳变过程和跳回过程,探讨在整个连续过程中圆柱壳上的应力分布情况,以及应力随时间和载荷变化的趋势,... 双稳态复合材料可广泛应用于各类可变结构的设计。针对反对称铺层的圆柱壳,利用有限元软件ABAQUS的Standard准静态分析,模拟其双稳态跳变过程和跳回过程,探讨在整个连续过程中圆柱壳上的应力分布情况,以及应力随时间和载荷变化的趋势,从而对该类可变结构的设计起到指导作用。结果表明:该类复合材料圆柱壳跳变过程中最大应力出现在载荷施加点与约束点附近,第二稳态下应力关于板中心呈中心对称分布,最大应力沿板壳对角线出现在四个角内侧附近,而跳回过程中应力由第二稳态下的分布慢慢变为集中在约束点附近。而且整个圆柱壳上的最大应力时刻与最大载荷施加的时刻不重叠,具有滞后性。 展开更多
关键词 碳纤维复合材料 有限元法 双稳态 von Mises应力 跳变 跳回
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热声载荷作用下薄壁结构非线性响应分析和试验验证 被引量:3
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作者 沙云东 张墨涵 +1 位作者 赵奉同 朱付磊 《航空学报》 EI CAS CSCD 北大核心 2019年第4期198-209,共12页
针对热声载荷作用下薄壁结构大挠度非线性响应问题,开展了固支约束金属薄壁板结构热声激励试验及数值模拟分析。通过计算结果与试验结果对比,表明两者结果存在一致性,进而验证了薄壁板在热声载荷作用下动态响应计算方法和数值模型的有... 针对热声载荷作用下薄壁结构大挠度非线性响应问题,开展了固支约束金属薄壁板结构热声激励试验及数值模拟分析。通过计算结果与试验结果对比,表明两者结果存在一致性,进而验证了薄壁板在热声载荷作用下动态响应计算方法和数值模型的有效性。在此基础上,针对加筋板结构完成了多种热声载荷组合作用下的动力学响应计算,获得了时域位移响应。重点对该结构在后屈曲状态下的3种典型振动形式进行分析,总结出热载荷与声载荷之间的相对强度决定了板的不同跳变形式。采用统计分析方法建立了位移响应的概率谱密度函数(PDF)并绘图,清楚地显示了后屈曲板的PDF表现出双峰现象。使用功率谱密度(PSD)函数分析了响应频率和峰值随着温度升高的变化,并确定了板的软化和硬化区域。总结了屈曲前/后结构特定区域拉应力和压应力的变化规律,并阐述了造成这种变化的原因。本文工作可对热声载荷作用下薄壁结构响应分析和动强度设计提供参考依据。 展开更多
关键词 薄壁结构 热声载荷 非线性响应 屈曲 跳变 试验验证
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