高速船复合材料层合板非线性动力响应分析

研究高速船复合材料层合板在冲击载荷作用下的非线性动力响应,其中位移和应力函数均用级数展开,应用四阶Runge-Kutta法进行数值求解,讨论了载荷形式对非对称复合材料层合板动力响应的影响。     

高速船复合材料层合板非线性动力响应分析

研究高速船复合材料层合板在冲击载荷作用下的非线性动力响应，其中位移和应力函数均用级数展开，应用四阶Runge-Kutta法进行数值求解，讨论了载荷形式对非对称复合材料层合板动力响应的影响。     

含分层损伤复合材料层合板频率响应函数分析

振动分析中含分层损伤复合材料层合板的动力特性是非常重要的，本文主要研究含分层损伤层合板的频率响应函数（FRFs)。首先，建立分层模型和基于FOSD理论的有限元层合板单元，为保证分析模型中避免出现上子板与下子板间的脱离或嵌入，引入了16节点虚拟界面罚单元，其次，根据Adams应变理论，由层合板SDC推导出相应结构振动的模态阻尼；最后，对0%-80%不同分层大小层合板的分析计算结果，讨论了不同分层大小对受损结构的固有频率，SDC和FRFs的影响，本研究不仅有助深入理解含分层复合材料层合板的动力特性，而且可发展用来预报复合材料层合板分层损伤的程度。     

水中含分层损伤复合材料层合板的声特征值研究

本文采用复合材料结构有限元和可压缩流体边界元耦合分析方法,研究了重流体介质(Heavy Fluid)中含层间分层损伤复合材料层合板结构的声特征值问题。在建立分析模型时,对完整与受损层合板结构采用有限元方法离散;而针对水中结构声辐射的特点,对可压缩流体介质中声压力场进行边界元离散,在此基础上讨论了含层间分层损伤复合材料层合结构的动力声特征值问题。文中给出的典型算例结果与参考文献结果吻合较好。同时以内含层间椭圆型分层损伤的复合材料层合板为典型结构,在重流体介质中探讨了影响结构声特征值的因素,本文工作为评判含层间损伤对其动力特征值的影响提供了一种有效的计算方法,而且也为含损伤复合材料层合结构声透射和辐射奠定了研究基础。     

含层间分层损伤复合材料层合板的动力响应研究

本文研究了含层间分层损伤复合材料层合板分层模型、阻尼和动力响应特征。在分层区上下子板间构造一种特定的界面连接单元,以防止分层处子板间的脱离或嵌入现象。为确定合理的有限元分析中的阻尼矩阵形式,文中进行了多种计算方式的比较,并做了T300/QY8911层合板梁的激振试验,依据耗散能等效,提出对阻尼矩阵构造的改良方法,使系统有限元动力响应分析中,既包含较多模态参数对结构响应的作用,又避免阻尼矩阵的满阵形式以利于有限元分析的计算机实施。利用时域直接积分法对稳态激励下的响应特征进行了研究,通过对界面连接单元刚度对动力特性影响的计算,给出分层受损复合材料层合板的动力响应特征,为含层间分层抽伤层合板动力分析提供了一个有效方法,同时,数值模拟结果对进一步理解层间分层损伤层合板的动态特性也存在一定的参考价值。     

风载作用下综合集成桅杆动态特性实验研究

综合集成桅杆采用复合材料层合板制造,在风载下的动力性能相比传统桅杆有很大改变.通过水池拖曳实验模拟桅杆受风载时的动力特性,测试压力和加速度等动态响应,分析复合材料层合板的力学特性,并与数值计算结果进行对比分析.结果表明:综合集成桅杆在迎风时的动力响应最大;桅杆复合材料层合板的实验值和计算值吻合良好,其应力值和位移值随载荷的增加呈线性变化,桅杆在流体中运动时不会发生共振.     

复合材料船体层合板的极限强度分析

基于更新拉格朗日格式,应用非线性层合三维退化壳元,结合有效的复合材料失效准则、刚度退化模型以及文中提出的刚度矩阵奇异判断准则,对复合材料层合板在轴向载荷作用下的轴向压缩极限强度问题进行深入研究.讨论了铺层方式、板厚等对极限强度的影响.通过与试验结果进行比较,表明基于文中提出的刚度矩阵奇异判断准则,结合增量更新拉格朗日格式下非线性层合三维退化有限元的计算方法能有效计算复合材料层合板的轴向压缩极限强度,并具有很高的精度.     

Analysis of impact damage characteristics of marine carbon fiber composite laminates embedded with PEI film北大核心CSCD

[目的]在传统船用碳纤维复合材料层合板层间添加热塑性相材料能有效提升船用复合材料的抗冲击性能,为探究其冲击损伤特性,开展实验研究。[方法]使用光学显微镜观察层合板的热塑性/热固性界面,分析两相材料的结合方式;对不同结构的复合材料层合板进行低、中、高3种不同能量的低速冲击;通过超声C扫描与电子显微镜,对各试件的损伤形貌进行观测,以研究各试件的冲击响应及损伤机理。[结果]结果显示,相较于碳纤维层合板,含热塑性相的船用复合材料层合板具有更好的损伤阻抗;内部嵌膜层合板试件在冲击能量为8和12 J的冲击下,内部分层损伤分别减少了19%和39%,且受到12 J冲击后,内部结构损伤较小,完整性较好。[结论]将PEI热塑性膜嵌于内部能提升层合板的韧性,显著减少内部分层损伤,明显提升内部嵌膜层合板的抗冲击性能。     

不同载荷形式下复合材料层合板渐进失效行为研究

近年来复合材料在船舶与海洋工程领域得到快速发展。船舶在服役周期内受载复杂,主要承载板材除受典型的面内拉压外载外,免不了遭受横向波浪载荷作用。研究复合材料层合板在不同载荷形式下结构的响应特征与损伤演化特性,有助于先进复合材料的性能评估及优化设计。本文采用三维实体单元及内聚力单元建立复合材料层合板模型进行计算分析,考察拉压载荷下层合板的极限承载能力与渐进失效过程,研究在横向载荷下层合板结构强度,对比分析其层内及层间损伤模式的差异性。     

复合材料桅杆层合板刚强度分析研究

针对封闭式桅杆中复合材料层合板结构进行设计,提出复合材料层合板结构设计方案。综合利用有限元软件ANSYS和相关强度准则对桅杆的复合材料部分进行强度和刚度校核,分析并总结出相关特性。确定并得出满足要求的复合材料层合板厚组合,实现复合材料桅杆的优化设计。并验证了设计的可行性,为复合材料桅杆以后的设计研究提供参考。     

Hydro-elastic analysis and optimization of a composite marine propeller

The present paper addresses the design and optimization of a flexible composite marine propeller. The aim is to tailor the laminate to control the deformed shape of the blade and consequently the developed thrust. The development of a hydro-elastic model is presented, and the laminate lay-up which minimizes the fuel consumption for the cruising and maximum speed conditions is simultaneously determined. Results show a reduction of 1.25% in fuel consumption for the combined case corresponding to a decrease of 4.7% in the cruising speed condition. Finally, the strength of the optimal blade is analyzed using the Tsai-Wu strength index. After local tailoring of the laminate configuration throughout the propeller a maximum value of 0.7 is determined indicating no failure will occur under normal operation conditions. The results suggest that it is possible to design a medium-sized flexible composite marine propeller that will enable a reduction of the fuel consumption while withstanding the imposed loads     

连续玄武岩纤维增强复合材料船体水下爆炸响应的数值仿真

运用有限元程序MSC.Dytran数值计算水下爆炸载荷作用下连续玄武岩纤维复合材料船体舱段结构的响应,采用层合板模型模拟纤维复合材料,选取一般耦合算法计算流体与结构的耦合效应,并将计算结果与E玻璃纤维复合材料船体仿真结果进行比较,分析2种材料船体结构压力时历曲线、破坏起始位置及破坏形式,得出结论:玄武岩纤维复合材料和E玻璃纤维复合材料船体底板在爆炸载荷的作用下起始破坏形式不同,玄武岩纤维的压缩强度和拉伸强度之比较高,在实际设计制造中更有优势。在船舶建造中可以使用连续玄武岩纤维复合材料替代玻璃纤维复合材料。     

Stress and failure analyses of thermoplastic composite pipes subjected to torsion and thermomechanical loading

The interest of using thermoplastic composite pipes has increased in offshore deepwater oil fields. Thermoplastic composite pipes consist of several carbon/glass fiber reinforced laminate layers to confer stiffness and strength located between inner and outer homogeneous thermoplastic layers for fluid containment and protection. This paper presents a theoretical analysis for thermoplastic composite pipes under combined pure torsion and thermomechanical loading from operational thermal gradients, considering the inner and outer isotropic homogeneous layers and intermediate transversely isotropic laminate ply layers. Perfect bond between adjacent layers and interfaces continuities are assumed. Based on the obtained stresses in the principal material directions, through-thickness failure indexes related to the von Mises and Maximum Stress or Tsai-Hill criteria are respectively evaluated for homogeneous and laminate layers. For each thermal gradient, the limit torque (i.e. when the failure index is equal to 1) is calculated. From the case study, it is observed that without thermal loading or for small operational temperature, failure occurs in the laminate, otherwise it is observed in the inner homogeneous layer. The thickness of the homogeneous layer significantly affects the limit torque and the absolute values of the limit clockwise and anticlockwise torque slightly differ when the operational temperature is included.     

水下爆炸脉动载荷对连续玄武岩纤维复合材料船体结构的影响

运用有限元程序MSC.Dytran模拟水下爆炸气泡脉动现象的整个过程,计算输出气泡中心位置压力时历曲线与爆炸理论吻合;采用层合板模型模拟连续玄武岩纤维复合材料,选取一般耦合算法计算流体与结构的耦合效应,计算连续玄武岩纤维复合材料舱段在脉动载荷作用下的动力响应;分析连续玄武岩纤维复合材料船体结构位移时历曲线、应力时历曲线及船底板应力云图.研究结果表明,在近场爆炸情况下,第一次脉动产生的应力波有可能比爆炸冲击波对船体造成更大的破坏;爆炸产生的脉动载荷频率接近整船或局部构件固有频率时,引发共振,对船体造成爆炸冲击破坏外的附加损害.     

正交各向异性圆柱壳的动力响应分析

从Fluegge关于圆柱壳的失稳方程出发,推导了正交各向异性圆柱壳在静水压力作用下,受到单位冲量作用的运动方程。本文使用模态叠加法求解瞬态响应方程,讨论了壳体参数和材料参数对于响应的影响,给出了部分结果。     

风帆辅助推进船舶操纵可控区研究

加装风帆后的船舶在低速时的航行特性有别于无帆情形。为确保低速航行安全,基于MMG非线性运动方程,计算了有、无风帆情况下的船舶操纵可控区。运动方程中的船体水动力系数、舵模块参数等由经验公式得到,帆/船整体气动力系数由基于滑移网格方法的CFD手段获得。计算结果表明:不同帆攻角下的船舶自由操控区不同,通过合理的帆/舵联合操纵,可以扩大风帆辅助推进船舶低速航行的可自由操控区,增强其在风中的抗风能力。     

循环荷载作用下加筋板格单元的损伤累积及力学模型研究

为了计算加筋板和船体梁在循环荷载作用下的极限强度,将一种能够考虑损伤累积和构件局部屈曲的一维钢材等效本构模型引入到加筋板格单元中,提出加筋板格单元在轴向循环荷载作用下的损伤累积力学模型,采用Visual Basic程序编制了计算程序,对若干加筋板格单元在双向轴向循环荷载作用下的承载性能进行计算研究,并使用非线性有限元软件Abaqus进行对比验证,结果表明所提理论方法具有较好的精度。     

含初缺陷损伤圆拱的动力屈曲

由Hamilton原理导出考虑初始缺陷及横向剪切变形时裂纹圆拱的动力屈曲控制方程;应用断裂力学中常用的线弹簧模型将裂纹引入到屈曲控制方程中;基于B-R动力屈曲判断准则,采用数值方法求解了受径向均布阶跃载荷作用时裂纹圆拱的动力屈曲;对比讨论了不同载荷幅值、裂纹长度、初始几何缺陷大小等因素对圆拱动力屈曲性能的影响.     

均布外压下球形封头屈曲特性研究（英文）

This study aims to experimentally and numerically examine the buckling performances of stainless steel spherical caps under uniform external pressure. Three laboratory-scale caps were fabricated, measured, and tested. The buckling behaviors of these caps were investigated through experiments and three numerical methods, namely, nonlinear Riks algorithm, nonlinear bifurcation, and linear elastic analysis. The buckling of equal-radius caps was numerically analyzed with different methods to identify their applicability under different wall thicknesses. The results obtained from the nonlinear Riks algorithm are in good agreement with the experimental results, which means the nonlinear Riks algorithm can accurately predict the buckling performances of spherical caps, including the magnitude of critical buckling loads and the deformation of post-buckling modes. The nonlinear bifurcation algorithm is only suitable for predicting the buckling loads of ultra-thin or large-span caps, and the linear buckling method is inappropriate for predicting the buckling of metal spherical caps.     

利用AGM求解粘弹性地基刚性梁的非线性控制微分方程（英文）

In the present paper a vibrational differential equation governing on a rigid beam on viscoelastic foundation has been investigated. The nonlinear differential equation governing on this vibrating system is solved by a simple and innovative approach, which has been called Akbari-Ganji’s method(AGM). AGM is a very suitable computational process and is usable for solving various nonlinear differential equations. Moreover, using AGM which solving a set of algebraic equations, complicated nonlinear equations can easily be solved without any mathematical operations.Also, the damping ratio and energy lost per cycle for three cycles have been investigated. Furthermore, comparisons have been made between the obtained results by numerical method(Runk45) and AGM. Results showed the high accuracy of AGM. The results also showed that by increasing the amount of initial amplitude of vibration(A), the value of damping ratio will be increased, and the energy lost per cycle decreases by increasing the number of cycle. It is concluded that AGM is a reliable and precise approach for solving differential equations. On the other hand, it is better to say that AGM is able to solve linear and nonlinear differential equations directly in most of the situations. This means that the final solution can be obtained without any dimensionless procedure.Therefore, AGM can be considered as a significant progress in nonlinear sciences.