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 共查询到19条相似文献,搜索用时 125 毫秒
1.
Phase change material(PCM) can be used to prepare the infrared false targets for realizing all-weather passive infrared decoy,but its low thermal conductivity is a great blockage to the simulation of the infrared signature of thick metal plates.For that reason,a method of simulating the infrared signature of thick steel plates by thermal conduction enhanced PCM,including the aluminum fins,is proposed.A physical and mathematic model is set up,and the infrared signature simulation of thick steel plate is investigated numerically.The effects of the distribution density and thickness of fins and the thickness of PCM plate on the simulation results are discussed,and the reasonable construction parameters of PCM plates used to simulate the steel plates of different thickness are obtained.  相似文献   

2.
The ability to predict the natural fragmentation of an explosively loaded metal casing would represent a significant achievement. Physically- based material models permit the use of small scale laboratory tests to characterise and validate their parameters. The model can then be directly employed to understand and design the system of interest and identify the experiments required for validation of the predictions across a wide area of the performance space. This is fundamentally different to the use of phenomenologically based material algorithms which require a much wider range of characterisation and validation tests to be able to predict a reduced area of the performance space. Eulerians numerical simulation methods are used to describe the fragmentation of thick walled EN24 steel cylinders filled with PBXN-109 explosive. The methodology to characterise the constitutive response of the material using the physically based Armstrong-Zerilli constitutive model and the Goldthorpe path dependent fracture model is described, and the results are presented. The ability of an Eulerian hydrocode to describe the fragmentation process and reproduce the experimentally observed fragment mass and velocity distributions is presented and discussed. Finally the suitability of the current experimental analysis methodology for simulation validation is addressed.  相似文献   

3.
4.
For the characterization of the behaviors of a metal material in events like expanding warheads, it is necessary to know its strength and ductility at high strain rates, around 104e105/s. The flyer plate impact testing produces the uniform stress and strain rates but the testing is expensive. The Taylor test is relatively inexpensive but produces non-uniform stress and strain fields, and the results are not so easily inferred for material modeling. In the split-Hopkinson bar(SHB), which may be used in compression, tension and torsion testing, the strain rates never exceeds 103/s. In the present work, we use the expanding ring test where the strain rate is 104e105/s. A streak camera is used to examine the expanding ring velocity, and a water tank is used to collect the fragments. The experimental results are compared with the numerical simulations using the hydrocodes AUTODYN, IMPETUS Afea and a regularized smooth particle(RSPH) software. The number of fragments increases with the increase in the expansion velocity of the rings. The number of fragments is similar to the experimental results. The RSPH software shows much the same results as the AUTODYN where the Lagrangian solver is used for the ring. The IMPETUS Afea solver shows a somewhat different fragmentation characteristic due to the node splitting algorithm that induces pronounced tensile splitting.  相似文献   

5.
In the measurement of damping material's dynamic mechanical performance (DMP) using flexural resonating cantilever beam method, the specimen's adhesive characteristic influences the test precision and accuracy. Taking its effect into account, the improved measurement equations based on the resonance method are presented. The simulated resuits show that, for the sake of weakening the adhesive's influence on the measured results, the adhesive should be spreaded as thin as possible when specimen is prepared, the adhesive's density and loss factor should be selected as small as possible also, and its Young's modulus should be selected according to the damping material being measured; the same adhesion condition effects differently on the test results of different damping materials, i.e. the error due to the adhesive is more inconspicuous if the damping layer has bigger thickness, modulus, loss factor and a certain density according to the damping material being measured. These conclusions provide theoretical basis for selecting adhesive, improving adhesion technology, and designing specimen.  相似文献   

6.
The notch tip fracture criterion of cored liner is proposed based on a dislocation model. The analysis reveals that the ductile shear fracture is a dominant fracture mode in the scored liner, and the fracture path is along the maximum shear stress tracing line. The numerical simulation of fracture process of scored liner under explosive loading is performed using the nonlinear finite element analysis program ANSYS-LS/DYNA, and then the experiments are made to verify the simulation. The experimental results are demonstrated to be in line with the numerical simulation results. The liner can form a focused jet of metal fragments with certain amount and mass that travels at very high speed in the cone-angle direction, which indicates that the dislocation model can be used to analyze the crack fracture of notch tip.  相似文献   

7.
When the mechanical drive is changed into the electric transmission,the cooling system of the engine compartment should be altered to meet the new requirement for the increasing in equipment such as electric apparatus.In order to predict and analyze the rationality of cooling system in the virtual engine compartment,the numerical simulation of airflow fields in the engine compartment by using computational fluid dynamics(CFD) technique is necessary.An armored vehicle with electric transmission in the research is taken as the research object.The physical model and mathematical model for the computation of 3D air flow and heat transfer in the engine compartment of an armored vehicle with electric transmission is established.Turbulent flow in the compartment is described by using the standard k-ε two-equation turbulence model.The temperature and velocity fields of 3D air flow in the engine compartment are numerically simulated and analyzed based on different fan's flux.A theoretical basis for determination of the fan's flux is given by the simulation results.The positions of the air-vent shutter are analyzed.The simulation results show that the different positions of the air-vent shutter can lead to different cooling efficiencies.  相似文献   

8.
A computational fluid dynamics (CFD) calculation model for the airflow and heat transfer in an armored vehicle cooling wind tunnel is established. A practical method to determine computation region outside power train compartment, produce grid and ensure grid quality is put forward. A commercial software FLUENT can be used to obtain solutions numerically in 3-D space. Precision of CFD calculation results is verified. The CFD model is used in designing a vehicle cooling wind tunnel, and air flow resistance of fan blast baffle is calculated. The calculated results show feasibility of the CFD rnodel and the method.  相似文献   

9.
Supersonic combustion of aviation kerosene is investigated under the flight conditions of Mach number 5 and fuel-air equivalence ratio 0. 551. The trajectories of the fuel droplets and the heat/mass transfer between them are simulated by means of discrete phase model (DPM). The k-ω model is chosen for turbulence closure and the non-premixed probability density function (PDF) approach is used to calculate the turbulence-chemistry interaction. The calculated wall static pressure and the total pressure loss coefficient are very close to the experiment results. The strut and cavity devices significantly increase the combustion efficiency.  相似文献   

10.
In order to evaluate the effects of the retarder on the braking stability quantitatively, an adhesion coefficient model is built for the composite braking produced by the retarder and the service braking system. The stability of composite braking is evaluated by using the model and the standard ECE R13. The evaluation results show that the composite braking stability decreases gradually with the increase of the retarder's braking force. To improve the stability, the braking force distribution of the service braking system is adjusted according to the position relationship among the braking force distribution line of the service braking system, the generalized braking force distribution line and the generalized I curve, and the constraints in ECE R13. The simulation results show that the composite braking stability can be improved significantly.  相似文献   

11.
导热增强型相变材料模拟钢板红外特征的优化设计   总被引:1,自引:0,他引:1  
叶宏  江利锋 《兵工学报》2007,28(6):692-699
相变材料( PCM)具有很大的相变潜热,应用于红外示假目标的制作可实现全天候被动式红外示假,但PCM的低导热系数是实现较厚金属板材红外特征模拟的一个主要障碍。针对这个问题,探讨利用铝肋片导热增强型PCM模拟钢板红外特征的方法,建立数理模型,对一系列厚度较大钢板的红外特征模拟进行数值计算,研究肋片的分布密度、厚度以及PCM的厚度等因素对模拟效果的影响,得到用于模拟不同厚度钢板红外特征的PCM板的合理结构参数。  相似文献   

12.
相变材料模拟金属板热特性的理论设计与实验验证   总被引:2,自引:2,他引:0  
采用一维热物理模型对相变材料板在不同季节模拟金属板的热行为特性进行了理论设计,优化出相变材料板的最佳厚度和物性参数。并以有机相变材料为研究对象,实验验证了设计的相变材料复合板能很好地模拟钢板的热行为特性。研究结果为相变材料应用于假目标提供了理论依据和关键材料。  相似文献   

13.
为了探究着靶角度对PELE侵彻钢筋混凝土靶扩孔效应的影响规律,建立了PELE侵彻钢筋混凝土靶的仿真模型,并且利用侵彻试验结果对仿真模型的准确性进行验证。在0~75°着靶角度范围内,从壳体变形模式、靶板扩孔直径等角度开展了PELE侵彻钢筋混凝土扩孔效应的影响规律与机理研究。研究结果表明:在0~30°着靶角度内,靶板的扩孔尺寸随着角度增大而增大,最大约为4.4倍弹径,并且PELE对钢筋混凝土靶板的破坏功增多; 随着着靶角度进一步增大,靶板的扩孔尺寸反而减小,PELE对钢筋混凝土靶板的破坏功也随之减少。此研究规律可对侵彻毁伤评估、新型动能武器系统设计提供技术支持和理论依据,并可用于指导钢筋混凝土防御工事设计。  相似文献   

14.
基于圆柱形空腔膨胀模型,将靶板变形所做的塑性功等效为刚性弹在整个侵彻过程所消耗的动能,对用于计算刚性卵形弹侵彻半无限厚铝合金靶板的侵深公式进行了推导。利用MTS万能试验机对2A12T4、6061T6、7075T6共3种铝合金材料进行了室温下的静态力学性能实验,得到了它们的真实应力-应变曲线,并将各参数代入侵深方程进行计算。通过12.7 mm穿燃弹侵彻3种铝合金靶板的末端弹道试验,得到了不同速度下3种铝合金靶板的侵彻深度,并与理论结果进行了对比验证。结果表明:该理论模型与试验结果吻合良好,推导得到的穿深方程较为可靠。同时,靶板材料的应力-应变数据的可靠性对模型预测的准确性有较大的影响。  相似文献   

15.
为研究7.62 mm穿甲弹垂直侵彻陶瓷金属复合靶板的弹道极限速度,基于能量守恒提出一种改进的理论分析模型,进行了7.62 mm穿甲子弹侵彻陶瓷/装甲钢复合靶板的试验研究,并通过理论分析的方法对试验结果进行验证计算。研究结果发现:陶瓷/装甲钢复合靶板利用该理论分析模型计算出的弹道极限速度与弹道试验结果吻合的较好;综合理论分析和数值模拟分析结果,得出弹道极限速度与陶瓷锥质量正相关。基于理论模型的可靠性,可预测不同复合靶板厚度下弹芯剩余高度,得出陶瓷厚度是决定弹芯剩余高度主要因素。  相似文献   

16.
本文介绍了一种箭载相控阵天线冷板的工作原理和结构形式,利用相变材料的原理,解决了箭载相控阵天线工作过程中T组件散热量大的问题。通过有限元分析和试验验证,表明冷板的设计切实可行。  相似文献   

17.
采用理论与实际相结合的方式,研究了热振环境下纤维增强悬臂复合薄板的振动响应。建立了热振环境下纤维增强悬臂复合薄板的理论模型,并考虑基础激励载荷的影响,利用双向梁函数法求解获得其振动响应。基于常温下测试获得的固有频率、阻尼比和模态振型来修正理论模型,以准确获得弹性模量、损耗因子等材料参数,并利用修正后的复合薄板理论模型来计算振动响应。搭建了热振环境下该类型复合薄板结构的振动测试系统,并以TC500碳纤维、树脂复合薄板为研究对象,进行了实际测试。测试结果表明,热振环境下悬臂复合薄板振动响应计算结果与测试结果的误差在1.4%~12.5%之间,进而验证了所提出的理论分析方法正确性。  相似文献   

18.
聚能射流对厚壁移动靶的侵彻理论与数值模拟分析   总被引:1,自引:0,他引:1  
贾鑫  黄正祥  徐梦雯  肖强强 《兵工学报》2019,40(8):1553-1561
为有效拦截摧毁来袭大壁厚高速运动的导弹和钻地弹,提出了一种采用破甲战斗部的攻击模式。基于虚拟源点理论并采用微元法,将射流微元与厚壁移动靶板的相互作用过程分为两个阶段: 第一阶段,射流微元在侵彻过程中不受靶板侧向力干扰,分析了该过程侵彻深度和孔径的变化规律;第二阶段,射流在侵彻过程中受到靶板的侧向干扰,建立了射流受干扰时的横向漂移速度及受干扰射流的侵彻深度等理论模型。为验证理论模型的正确性,设计了一种40 mm口径聚能装药,通过有限元软件LS-DYNA分析了聚能射流垂直侵彻不同移动速度靶板(0~600 m/s)的侵彻深度及孔径变化规律,同时结合Marmor等\[17\]的试验数据,与所建理论模型计算结果进行对比。结果表明:破甲战斗部是对付高速运动厚壁战斗部的有效手段,所建理论模型可精确地计算出射流微元在各个阶段的运动状态,从而获得总侵彻深度随靶板运动速度变化的规律;靶板运动速度越高,无干扰侵彻阶段经历时间越短,射流受干扰程度越明显,破甲深度与扩孔孔径也越小。  相似文献   

19.
为加强装甲目标的防护能力及提高靶板的抗侵彻性能,对弹丸侵彻双层不同材质靶板进行数值模拟。建 立弹丸侵彻靶板的几何和仿真模型,采用ANSYS/LS-DYNA 软件,比较了3 种不同材料靶板的抗侵彻能力,对不 同材质的双层有、无间隔靶板组合的抗侵彻性能进行数值模拟,并对比了靶板排列顺序不同对靶板组合抗侵彻性能 的影响。模拟结果表明:双层不同材质的靶板组合的抗侵彻能力与两层靶板的材质和排列方式有关,双层间隔靶板 组合比双层无间隔靶板组合的抗侵彻性能更好。  相似文献   

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