Numerical simulation on truncated oval-nosed projectile penetrating into stiffened plate北大核心CSCD

[Objectives]In this paper, the numerical simulation method is used to study the anti-penetration performance and energy absorption mode of a stiffened plate, as well as the influence of different stiffened bars on the flight attitude of the projectile body.[Methods] Finite element software LS-DYNA is used to simulate the process of a truncated oval-nosed projectile penetrating a stiffened plate, and the results of the numerical simulation are compared with an experiment to verify the reliability of the numerical simulation method. The momentum method and mass equivalence method are used to predict the residual velocity of the projectile, and the applicability of different theoretical methods within different velocity ranges is compared. The deformation energy of different regions of the stiffened plate is then extracted to analyze the influence of the initial velocity of the projectile body on the energy absorption mode of the target plate. Finally, the structure of the stiffeners is changed and the influence of the relative position of the stiffeners on the penetration attitude of the projectile body is analyzed.[Results]The results show that the mass equivalence method is more accurate than the momentum method in predicting the residual velocity of the stiffened plate when the initial velocity of the projectile body is in the range of 300–900 m/s. The ratio of the deformation energy of the stiffened plate to the energy loss of the projectile body decreases with the increase of the initial velocity of the projectile body. The effect of a T-stiffened plate on trajectory is greater than that of a rectangular-stiffened plate.[Conclusions]The related calculation method and research results have certain reference value for research and engineering application surrounding the anti-penetration of stiffened plates. © 2023 Chinese Journal of Ship Research. All rights reserved.     

Research on the fragment impact resistance of a composite mast

Due to the unique structural mode and material property of a composite sandwich plate, related research such as fragment impact resistance of a composite mast is short of publication and urgent in this field. In this paper, the commonly accepted sandwich core board theory was modified. Damage caused by a fragment attack was simulated onto a sandwich plate model built with solid and shell elements. It was shown that shear failure and vast matrix cracking are the main reasons for outer coat damage, and tension failure and partial matrix cracking are the cause for inner coat damage. Additionally, according to complexities in actual sea battles, different work conditions of missile attacks were set. Ballistic limit values of different fragment sizes were also obtained, which provides references for enhancing the fragment impact resistance of a composite mast.     

质量比对于柔性圆柱体流激振动的影响（英文）

The effect of the mass ratio on the flow-induced vibration(FIV) of a flexible circular cylinder is experimentally investigated in a towing tank. A Tygon tube with outer and inner diameters of 7.9 mm and 4.8 mm, respectively, was employed for the study. The tube was connected to a carriage and towed from rest to a steady speed up to 1.6 m/s before slowing down to rest again over a distance of 1.6 m in still water. Reynolds number based on the cylinder's outer diameter was 800–13,000, and the reduced velocity(velocity normalized by the cylinder's natural frequency and outer diameter) spanned from 2 to 25. When connected, the cylinder was elongated from 420 mm to 460 mm under an axial pre-tension of 11 N. Based on the cylinder's elongated length, the aspect ratio(ratio of the cylinder's length to outer diameter) was calculated as 58. Three mass ratios(ratio of the cylinder's structural mass to displaced fluid mass, m*) of 0.7, 1.0, and 3.4 were determined by filling the cylinder's interior with air, water, and alloy powder(nickel-chromium-boron matrix alloy), respectively. An optical method was adopted for response measurements. Multi-frequency vibrations were observed in both in-line(IL) and cross-flow(CF) responses; at high Reynolds number, vibration modes up to the 3rd one were identified in the CF response. The mode transition was found to occur at a lower reduced velocity for the highest tested mass ratio. The vibration amplitude and frequency were quantified and expressed with respect to the reduced velocity. A significant reduced vibration amplitude was found in the IL response with increasing mass ratios, and only initial and upper branches existed in the IL and CF response amplitudes. The normalized response frequencies were revealed to linearly increase with respect to the reduced velocity, and slopes for linear relations were found to be identical for the three cases tested.     

基于改进的Logvinovich法对带横摇运动非对称楔形体入水砰击力的计算(英文)

The water entry problem of an asymmetric wedge with roll motion was analyzed by the method of a modified Logvinovich model (MLM). The MLM is a kind of analytical model based on the Wagner method, which linearizes the free surface condition and body boundary condition. The difference is that the MLM applies a nonlinear Bernoulli equation to obtain pressure distribution, which has been proven to be helpful to enhance the accuracy of hydrodynamic loads. The Wagner condition in this paper was generalized to solve the problem of the water entry of a wedge body with rotational velocity. The comparison of wet width between the MLM and a fully nonlinear numerical approach was given, and they agree well with each other. The effect of angular velocity on the hydrodynamic loads of a wedge body was investigated.     

阻振质量参数对动力舱段隔振性能影响规律研究

Rigid blocking masses are located in the typical base structure of a power cabin based on the impedance mismatch principle.By combining the acoustic-structural coupling method and statistical energy analysis,the full-band vibration and sound radiation reduction effect of vibration isolation masses located in a base structure was researched.The influence of the blocking mass’ cross-section size and shape parameters and the layout location of the base isolation performance was discussed.Furthermore,the effectiveness of rigid vibration isolation design of the base structure was validated.The results show that the medium and high frequency vibration and sound radiation of a power cabin are effectively reduced by a blocking mass.Concerning weight increment and section requirement,suitably increasing the blocking mass size and section height and reducing section width can result in an efficiency-cost ratio.     

Control of Vortex Shedding and Drag Reduction through Dual Splitter Plates Attached to a Square Cylinder

In this paper we have made a numerical study on the control of vortex shedding and drag reduction of a cylinder by attaching thin splitter plates. The wake structure of the cylinder of square cross-section with attached splitter plates is analyzed for a range of Reynolds number, based on the incident stream and height of the cylinder, in the laminar range. The Navier-Stokes equations governing the flow are solved by the control volume method over a staggered grid arrangement. We have used the semi-implicit method for pressure-linked equation(SIMPLE) algorithm for computation. Our results show that the presence of a splitter plate upstream of the cylinder reduces the drag, but it has a small impact on the vortex shedding frequency when the plate length is beyond 1.5 time the height of the cylinder. The presence of a downstream splitter plate dampens the vortex shedding frequency. The entrainment of fluid into the inner side of the separated shear layers is obstructed by the downstream splitter plate. Our results suggest that by attaching in-line splitter plates both upstream and downstream of the cylinder, the vortex shedding can be suppressed, as well as a reduction in drag be obtained. We made a parametric study to determine the optimal length of these splitter plates so as to achieve low drag and low vortex shedding frequency.     

Bandgap optimization for chiral acoustic metamaterials based on material selection method北大核心CSCD

［Objectives］This study seeks to expand the bandgap frequency band, reduce the bandgap starting frequency and analyze and optimize the bandgap parameters of acoustic metamaterials. ［Methods］The influence of geometrical and material parameters on the bandgap properties of acoustic metamaterials is analyzed, and a method for maximizing the bandgap width is proposed. The multi-objective optimization problem is converted into a single objective optimization problem by normalizing the bandgap frequency coefficients. Structural material conversion is achieved via the material selection optimization method, and the optimization equations of bandgap parameters are established on the basis of weight-lightening. For chiral acoustic metamaterials, the material properties (density and wave velocity) and geometric parameters (scatterer diameter, ligament thickness and coating thickness) are defined as design variables, and the comprehensive optimization of structural parameters and material selection of acoustic metamaterials based on weight-lightening are implemented. ［Results］The optimization results show that the bandgap width increases by 27.7% and the lower bound frequency decreases by 1048 Hz, thereby achieving the goal of expanding the bandgap width based on lightweight acoustic metamaterials. The acoustic transmission analysis of the finite chiral acoustic metamaterial structure is then carried out to verify the effectiveness of the proposed method. ［Conclusions］The results show that the goal of lightweight acoustic metamaterials can be effectively achieved by integrating the comprehensive optimization of structural parameters and materials. As such, this study provides references for the design of new-type acoustic metamaterials. © 2023 Authors. All rights reserved.     

粘流方法的螺旋桨尾流场数值分析(英文)

The computational fluid dynamics(CFD) method is used to numerically simulate a propeller wake flow field in open water.A sub-domain hybrid mesh method was adopted in this paper.The computation domain was separated into two sub-domains,in which tetrahedral elements were used in the inner domain to match the complicated geometry of the propeller,while hexahedral elements were used in the outer domain.The mesh was locally refined on the propeller surface and near the wake flow field,and a size function was used to control the growth rate of the grid.Sections at different axial location were used to study the spatial evolution of the propeller wake in the region ranging from the disc to one propeller diameter(D) downstream.The numerical results show that the axial velocity fluctuates along the wake flow;radial velocity,which is closely related to vortices,attenuates strongly.The trailing vortices interact with the tip vortex at the blades’ trailing edge and then separate.The strength of the vortex shrinks rapidly,and the radius decreases 20% at one diameter downstream.     

声传输进结构-声腔耦合舱室空间的主动控制策略和机理研究(英文)

An analytical study was presented on active control of sound transmission into a vibro-acoustic enclosure comprising two flexible plates. Two types of actuators were used, i.e. acoustic actuator and distributed lead zirconate titanate piezoelectric (PZT) actuator instead of point force actuator. Using the modal acoustic transfer impedance-mobility matrices, the excitation and interaction in the coupled sound transmission system can be described with clear physical significance. With the control system designed to globally reduce the sound field, different control system configurations were considered, including the structural actuator on the incident plate, actuator on the receiving plate, acoustic actuator on the cavity, and their combinations. The effectiveness and performance of the control strategy corresponding to each system configuration were compared and discussed. The role and control mechanism of each type of actuator were of particular interest. It was shown that the incident plate actuator is effective in controlling the cavity-dominated modes and the structural modes dominated by the incident plate and receiving plate. Two main control mechanisms are involved in this control configuration, i.e., modal suppressing and modal rearrangement. For control system configuration with only acoustic actuator in the enclosure, the mechanism involved in this arrangement is purely modal suppression. Desirable placements of structural actuators in terms of total potential energy reduction were also discussed.     

舰船舷侧防爆结构在内部爆炸作用下破裂的数值模拟

文章通过应用MSC.Dytran中的多欧拉一拉格朗日耦合方法,对反舰武器战斗部进入舷侧防爆结构内部爆炸作用下其变形和破坏的情况进行数值模拟研究.用多欧拉域模拟结构内外空气中爆炸冲击波传播情况.用快速一般耦合方法计算结构和流体的耦合作用.模拟结果显示:在冲击波作用下,防护结构外层舱室变形、失效后破裂,冲击波通过破口流入内层舱室.由于文中考虑了结构破坏与爆炸冲击波的相互作用,使得数值模拟方法和结果更符合实际.通过对爆炸冲击波动能与结构吸能的研究发现,除了结构的直接吸收削弱了冲击波的动能以外,通过破孔和舱壁上预开的孔泻掉的能量相当于结构总吸能的46.7%.因此在舰船舷侧防护结构设计时考虑内舱壁的适当开孔并减小强度是有益和必要的.     

舰船舱室内部爆炸的数值模拟研究

反舰武器战斗部在舰船舷侧防护结构内部爆炸将造成舱室的严重破坏,数值模拟是分析结构在爆炸载荷作用下破坏情况的有效手段之一.舱室内部爆炸的数值模拟涉及到冲击波传播、多个流场与结构的耦合、结构的变形与破坏.文章基于MSC.Dytran软件平台,实现了舱室内部爆炸的数值模拟.研究表明,在舱壁开口有利于减小舱室角隅处的汇集压力,保护舱室结构.同时,爆炸产生的二次破片对舱室结构能产生进一步毁伤效果.     

复合材料吸声系数的理论计算及性能分析

不同噪声环境中的降噪需求不同,为根据噪声频谱合理设计复合吸声材料,基于穿孔板及多孔吸声材料的吸声原理,提出了改进的声-电类比法,推导出复合吸声材料吸声系数的理论计算公式.利用该种计算方法,通过数值仿真深入分析复合吸声材料内外层穿孔率,多孔材料厚度,空腔变化对吸声性能的影响,分析表明第1层板穿孔率及多孔材料厚度影响较大.最后用声学实验对计算结果进行验证,表明改进的声-电类比法有效.     

舰船防护水舱在接近爆炸载荷作用下响应的理论研究

防护水舱作为抵御反舰武器爆炸破片和冲击波效应的有效手段之一,在舰船防护结构中经常被采用.爆炸冲击波是一种瞬态的作用,水舱在这种瞬态冲击载荷作用下的响应涉及内、外板以及舱内水的相互作用,其响应机理十分复杂.迄今为止人们还没有对其进行比较完整和严格的理论分析.文章通过适当的假设,对防护水舱内外舱壁在接近爆炸载荷作用下的响应机理进行了理论分析,推导出了水舱内、外板的响应计算公式,并做了算例研究.文中的研究对防护水舱这种特殊结构抵御爆炸冲击波的机理有了进一步的理论解释,并对其设计提出了可供参考的依据和原则.     

水下爆炸冲击波作用下船体舱段变形试验研究

对舰船实尺度舱段在水下爆炸载荷作用下的船底板架变形进行了试验研究及理论分析。以舱段在水下爆炸的试验现象及结果为基础,通过平板模型求解药包在水下任意位置爆炸时舱段的刚体运动特性,以冲击波的入射能减去舱段刚体运动动能作为船底板架的弹塑性变形能,利用能量法,对船底板架应用薄板的大挠度弯曲理论进行局部变形求解。试验结果及理论分析表明:舱段模型在水下爆炸过程中会产生较大的刚体运动,船底外板变形区域主要集中在纵桁和实肋板交叉的板格内,理论求解的板格最大变形与试验结果较为一致。该文结果可对船体外板变形计算及局部强度考核提供数据及理论的参考。     

破片高速侵彻防护液舱剩余特性研究

为探讨破片高速侵彻液舱后的剩余特性,通过弹道试验,并结合有限元分析软件Ansys/Ls-Dyna,比较破片侵彻垂直和倾斜液舱后的瞬时余速和运动轨迹.试验结果表明:破片穿透液舱前板初期,会产生空泡和射流,空泡大小和射流强度与破片入水初速有关,而空泡形状和射流方向则受液舱的倾斜角度影响;破片穿透液舱前板后,在水中的运动轨迹会发生偏转,偏转方向与破片入水初速有关.     

舰船RCS整形设计中的电磁分析

减小舰船雷达散射截面（RCS）需要对舰船进行整形设计。本文从分析舰船典型结构——金属板的RCS与雷达波的入射角、频率及几何尺寸的关系出发,采用物理光学法导出了金属平板RCS与倾斜角的理论公式,确定了在单频点或多频点对平板进行雷达隐身设计的最佳倾斜角,通过具体实例说明了在舰船整形设计时,采用本文给出的计算公式可以对舰船的RCS和舱室容积进行折衷设计。结论对舰船雷达隐身设计具有指导意义。     

舱室爆炸载荷作用下舷侧防护结构的响应研究

文章对舱室爆炸载荷作用下舷侧防护结构的响应进行了研究,对防护结构的破坏形式、纵舱壁的响应等进行了详细分析.在舱室爆炸载荷作用下,防护结构中以膨胀舱的受损程度最为严重,液舱往里结构受损程度较轻.受膨胀舱中隔板间距疏密影响的,主要是膨胀舱中甲板及横舱壁,液舱往里结构所受影响很小.     

水面舰艇舷侧防雷舱结构水下抗爆防护机理研究

在文献[1]朱锡等人关于水面舰艇舷侧防雷舱结构模型抗爆试验研究结果的基础上,分析了水面舰艇舷侧防雷舱各层防护结构在舷侧遭受水中兵器接触爆炸时的破坏模式,从能量的角度计算了各个防护层的吸能率.提出能量流的概念,揭示了水面舰艇舷侧防雷舱的防护机理,从而为防雷舱的防护设计提供了理论基础.     

多层防护结构舱内爆炸试验

舰船舷侧多层防护结构的主要作用是抵御反舰武器对内部结构的破坏。文章通过反舰武器战斗部模型在舰船舷侧防护结构内部爆炸的模拟试验,研究了战斗部内爆作用下防护结构的破坏模式、多层防护结构防御冲击波和高速破片的效果以及内部结构的冲击响应,对比分析了空舱和水舱在战斗部接近爆炸作用下的变形和破坏情况。通过对试验数据的分析发现在战斗部接近爆炸载荷作用下,水舱内板的动态响应出现了"二次加载"现象。