共查询到19条相似文献,搜索用时 140 毫秒
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首次采用首部钢丝绳牵引方式进行了超空泡流下壳结构模型实验。实验模型壳体部分采用聚碳酸酯材料,锥部采用铝合金材料,首部空化器则采用不锈钢制作,最后各部分通过螺纹或者胶水粘结而成。三种不同速度下的超空泡实验结果表明:采用首部钢丝绳牵引方式进行超空泡实验是可行的。位于壳体上相对位置相同的部位其应变曲线趋势一致,超空泡形成后轴向的减阻效果是非常明显的,尾拍振动引起的应变则呈现出周期性的特征。在一定速度下,超空泡形成后轴向力引起的应变和尾拍振动引起的应变处于同一个水平上。随着速度的提高,超空泡减阻的效果更加明显,尾拍振动引起的应变幅值也相应增大。实验结果可为超空泡水下航行体的结构设计提供依据。 相似文献
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为研究空化器形状对超空泡射弹尾拍航行时运动特性的影响,基于有限体积法和Mixture多相流模型,结合动网格技术构建了三维自由尾拍运动仿真模型,在两种长径比下比较了平头弹、凹口弹、锥头弹的尾拍运动特性,并分析了其水动力影响因素。结果表明:较小长径比下,平头弹可以保持运动稳定,凹口弹和锥头弹易失稳,主要是由于空化器产生的空泡尺寸差异导致其临界失稳攻角依次降低。较大长径比下,临界失稳攻角消失,三种头型射弹均能保持尾拍稳定,锥头弹在速度较高时以“单侧尾拍”保持稳定,速度降低后以“双侧尾拍”保持稳定,而平头弹和凹口弹始终以“双侧尾拍”保持稳定;锥头弹由于“单侧尾拍”会产生与初始扰动方向相反的垂直位移,而平头弹和凹口弹由于弹头升力产生与初始扰动方向相同的垂直位移。 相似文献
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该文建立了描述结构大变形和主缆初始曲率产生的几何非线性对系统动力学影响的悬索承重梁索耦合结构垂向运动动力学偏微分方程组。通过Galerkin方法一次截断把偏微分方程组化为时域上的两自由度常微分方程组。使用多尺度法得到简谐激励下常微分方程组主共振时的一次近似解。结果显示,当外激励仅激发低频或高频主共振时,系统的振幅随激励的幅值或激励频率的变化出现突然的跳跃。当激励同时激发低频和高频主共振时则有两种情况:1) 若固定高频激励幅值和频率,则系统的低频和高频振动成分的振幅随低频激励参数变化同时增加或减小;2) 若固定低频激励的幅值和频率,则系统的低频和高频振动成分的振幅随高频激励参数变化以相反的趋势变化。即高频振动幅值增大时,低频振幅减小,反之亦然。 相似文献
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以电磁开关系统为研究对象,根据拉格朗日麦克斯韦方程建立三阶非线性动力学模型,应用MLP法得到电磁开关强非线性系统主共振的幅频响应方程及位移和电流分别随时间变化的振动规律,分析系统各参数对系统主共振幅频响应曲线的影响。结果表明,系统的幅频响应曲线存在跳跃现象;随着阻尼系数的增大,系统的振幅减小;随着激励电压幅值增大,系统的振幅和共振区域增大;随着电阻增大,系统的振幅和共振区域减小。 相似文献
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针对TBM破岩过程产生基础振动对液压胶管内流体动态特性影响,根据层合板理论建立缠绕式液压胶管振动梁模型,并结合轴向流固耦合模型建立胶管轴向振动动力学模型。运用特征线法求解该数学模型,研究基础振动参数和胶管结构参数对流体响应特性影响,发现胶管出口压力波动幅值随基础振动振幅呈线性增加的趋势,随振动频率增加,在40 Hz左右达到最大,此时振动频率接近系统固有频率;胶管出口压力峰值随液压胶管长度增加而减小,胶管内径在8 mm到30 mm变化时,其先增大后减小,随泊松比增大而增大。研究结果表明振动沿胶管轴向分量加强了流体与胶管互动效应,可为TBM液压管系设计和抗振提供理论依据。 相似文献
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以同一轴线上双激振器驱动的振动磨机为典型研究对象,通过对其实际模型的合理简化,得到运动系统的力学模型.利用Lagrange方程建立了运动系统的动力学方程,通过对动力学方程的求解分析,得到了振动体的运动轨迹随两个激振器转角差的变化规律,振动体在运动过程中,随着两个激振器转角差的增大,振动体质心的运动幅值减小,而沿质心轴线两端的运动幅值增大,当两个激振器转角差达到180度时,质心运动幅值为零,沿质心轴线两端的运动幅值达到极大,此时振动系统产生锥形运动,使得振动设备无法正常工作.研究结果可为研究更复杂振动系统的同步运动和利用同步运动减少参振体质量提供理论基础. 相似文献
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Mass abrasion is observed on the nose of projectile when a projectile strikes concrete target at high velocity. To evaluate the influence of the mass abrasion on the depth of penetration (DOP) limit, the relationship between the nose factor of the residual projectile after abrasion and the initial impact velocity is suggested according to the experimental data. Based on the dynamic cavity expansion theory, with considering the effects of varying nose factor and mass of projectile, a modified model is proposed to calculate the depth of penetration of kinetic energy penetrator. The model predicts that a theoretical maximum DOP exists due to the mass abrasion of the projectile. The model is checked by the different experimental data. 相似文献
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为了提高通气超空泡航行体在转弯运动过程中空泡和航行体的运动一致性,基于有限体积法和VOF多相流模型,采用动态网格技术对航行体转弯运动的空泡形态特性进行了非定常数值模拟研究。通过对航行体沾湿区域的分析,揭示了沾湿区域形成的原因,利用空化器对空泡轴线的定向效应,提出了合理改变侧滑角减缓沾湿区域出现的具体方法。通过分析侧滑角和侧滑角速度对航行体沾湿区域的影响,提出了超空泡航行体转弯运动过程中,在给定偏航角条件下避免出现沾湿区域的侧滑角和侧滑角速度的适用范围,为进一步研究超空泡航行体机动运动问题提供参考。 相似文献
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The problems of optimum distribution of active stiffeners manufactured from piezoelectric or shape memory alloy materials and bonded to or embedded within the facings of a sandwich plate are considered. The sandwich plate consists of thin composite or isotropic facings which are in the state of plane stress and a thick shear deformable core. The amplitude of forced vibrations of the plate is reduced using symmetric couples of piezoelectric stiffeners subjected to out-of-phase dynamic voltages. Shape memory alloy stiffeners are used to reduce bending deformations. In the latter case, a desirable effect is achieved by activating the stiffeners on one side of the middle surface. Optimum design is considered based on the requirement of minimal transverse static or dynamic deflections subject to a constraint on the volume of smart stiffeners. The variables employed in the process of optimization are the ratios of the cross-sectional areas of the stiffeners in each direction to their respective spacings. It is shown, that, dependent on the load, materials, and geometry, optimum design can significantly reduce deflections, i.e. enhance the strength, of sandwich plates. 相似文献
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GUO Zheng-yu ZHANG Yu-wen FAN Hui College of Marine Engineering Northwestern Polytechnical University Xi′an China 《国际设备工程与管理》2009,14(1)
The cavitator is the key component of a supercavitating vehicle. Based on the potential flow theory and ANSYS, we perform stress and deformation analysis of a cavitator and present a computational procedure of supercavitating shape when the vehicle was in high speed motion. Different shapes and materials models were examined to determine the deformation and the extent of influence on the cavity shape. Information obtained from these analyses reveals that the deformation of the cavitator can be one of the ca... 相似文献
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The present research deals with the study of buckling pressure-to-weight ratio of cylindrical shells with laminated ring stiffeners. The research introduces a strain energy formulation for laminated rings, in which each ring stiffener may be treated individually and the geometrical dimensions and material properties of the stiffeners may be different from one another. In a parametric study, the impacts of various geometrical parameters of rings on the buckling pressure-to-weight ratio of shells for composite and metallic stiffeners are compared. The results show that the buckling-to-weight behavior of the shells with Steel stiffeners generally differs from the shells with stiffeners made of Aluminum, E-glass/epoxy, Graphite/epoxy, or Kevlar49/epoxy. 相似文献
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The average force acting on a cylindrical or spherical body placed near the boundary of cylindrical cavity filled with liquid and executing rotational vibrations is experimentally studied. The repulsive lift force acting on solid is found and measured using the method of body suspension in the gravity field. In horizontal cavity the repulsive force provides steady state of light cylinder near the upper boundary at a distance comparable with the thickness of the Stokes layer. The heavy sphere which hangs on thread repulses from the wall of vertical cylindrical cavity under torsional vibration. The dependence of the average lift force on the amplitude and frequency of vibrations and on distance between the body and the boundary has been investigated. Results are presented on the plane of dimensionless parameters. In the examined frequency range the lift force acting on cylinder decreases exponentially with distance from the boundary. Lift force acting on sphere decreases with distance and strongly depends on dimensionless frequency of vibration. Conclusion that lift force is generated by body oscillations excited by its viscous interaction with the oscillating boundary is done. The found phenomenon is important for control of inclusions under microgravity conditions. 相似文献
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通过对变速超空泡水下航行体壳结构受力模型的分析,建立了恒定推力下航行体的平面运动方程,确定了变速过程中的阻力和冲击力。利用有限元方法,进行了结构响应计算,分析了减速过程中节点时域上的最大应力值在轴向的分布情况及典型节点处的响应。结果表明:航行体所需推力和所受应力较大,对其结构强度要求较高;运动过程中,节点时域上的最大应力在空间域上的极大值主要分布在首尾端部和柱壳中部;存在一些振动频率对航行体结构响应影响显著。结果对超空泡航行体壳结构受力和强度分析以及优化设计有着重要的指导意义。&;#61472; 相似文献