A study on the surface overpressure distribution and formation of a double curvature liner under a two-point initiation

The formation mechanism of an EFP(explosively formed projectile) using a double curvature liner under the overpressure effect generated by a regular oblique reflection was investigated in this paper.Based on the detonation wave propagation theory,the change of the incident angle of the detonation wave collision at different positions and the distribution area of the overpressure on the surface of the liner were calculated.Three-dimensional numerical simulations of the formation process of the EFP with tail as well as the ability to penetrate 45# steel were performed using LS-DYNA software,and the EFP ve-locity,the penetration ability,and the forming were assessed via experiments and x-ray photographs.The experimental results coincides with those of the simulations.Results indicate that the collision of the detonation wave was controlled to be a regular oblique reflection acting on the liner by setting the di-mensions of the unit charge and maintaining the pressure at the collision point region at more than 2.4 times the CJ detonation when the incident angle approached the critical angle.The distance from the liner midline to the boundary of the area within which the pressure ratio of the regular oblique reflection pressure to the CJ detonation pressure was greater than 2.5,2,and 1.5was approximately 0.66 mm,1.32 mm,and 3.3 mm,respectively.It is noted that pressure gradient caused the liner to turn inside out in the middle to form the head of the EFP and close the two tails of the EFP at approximately 120μs.The penetration depth of the EFP into a 45# steel target exceeded 30 mm,and there was radial expansion between the head and tail of the EFE increasing the penetration resistance of the EFP.Therefore,the structural size of the unit charge and the liner can be further optimized to reduce resistance to increase the penetration ability of the EFP.     

The investigation of NTO/HMX-based plastic-bonded explosives and its safety performance

3-nitro-1,2,4-triazol-5-one (NTO) is the main component of insensitive munitions (IM) formulation because of its outstanding insensitive properties.In this paper,a series of NTO/HMX-based composite explosives were prepared and characterized.The study focuses on the effect of NTO on the performance of the formulations,especially the safety performance.The results revealed that the mechanical sensi-tivity of formulations was associated with NTO content,as well as the thermal conductivity,specific heat capacity and Arrhenius parameters.Then,the high amount of NTO using in formulation was proved to be helpful for NTO/HMX-based formulation to exhibit good thermal safety.Besides,by accelerating rate calorimeter (ARC) and a modified cook-offequipment,the pressure and pressure rise rate were proved as the important indicator for judging the thermal safety performance in confined spaces.Finally,the numerical simulation was used as a credible method for predicting the respond temperature of cook-off experiment.     

高功率密度柴油机热部件散热量MAP研究

为满足某型高功率密度柴油机智能化控制冷却系统的设计需要,构建了高功率密度柴油机与冷却系统的工作过程耦合模型。利用该模型计算了柴油机关键热部件的散热量MAP,并对结果进行了分析。结果表明:一级中冷和二级中冷散热量随环境温度升高而降低;级间中冷散热量随环境温度的升高而升高。应用该方法能够快速掌握高功率密度柴油机的散热规律,为制定智能化控制冷却系统的控制策略提供依据。     

尾流自导鱼雷带角射击弹道仿真

为简化指控系统解算流程,缩短指控系统解算尾流自导鱼雷带角射击参数时间,为后续的鱼雷模拟器的软件研制提供实现手段,提出在尾流自导鱼雷有利提前角射击弹道的基础上进行二次转角航行的改进的尾流自导鱼雷带角射击模型。依据尾流自导鱼雷射击原理,结合有利提前角射击和二次转角射击,对所提出的模型及其约束条件进行了分析与推导,简化了鱼雷带角射击参数的解算。深入分析了尾流自导鱼雷带角射击逻辑,提出采用面向过程设计方法对模型进行仿真,经过对仿真输出图形和仿真数据的分析,验证了所提出模型的准确性。     

基于SAR的装备维修手册生成技术

保障性分析记录(Supportability Analysis Record,SAR)是维修手册编写的基础数据来源,针对传统纸质维修手册存在的缺陷以及维修手册编写中SAR的利用率不高等问题,提出了以保障性分析记录建立底层数据环境直接生成维修手册的设计思想,构建了基于SAR的装备维修手册生成技术框架,突破了基于XML的SAR表示技术。该框架充分利用SAR数据生成维修手册,提高了分析数据的可重用性,避免了重复分析,降低了工作量,提高了维修手册生成效率。     

空间重采样的宽带多重信号分类算法高分辨方位估计

空间重采样法是宽带恒定束宽波束形成的一种重要方法,采用声矢量阵推导了基于空间重采样的宽带MUSIC算法,并和相干子空间FFT插值法做了仿真比较,结果表明,所提算法的性能优于FFT插值法,表现为更低的分辨信噪比门限和估计均方误差上.     

高重合度人字齿轮轮齿最佳修形优化设计

基于斜齿轮轮齿接触分析技术,建立了考虑人字齿轮典型安装误差的抛物线人字齿轮轮齿接触分析方法。综合考虑人字齿轮的传动误差与啮合特性,采用带精英策略的快速非支配排序遗传算法对高重合度人字齿轮的传动性能进行了多目标优化设计,该算法克服了优化结果的局部收敛,获得了人字齿轮最佳的齿廓、齿向抛物线修形参数。通过实例表明,修形优化后的齿面啮合印痕与传动误差较优化之前得到了明显的改善,有效地改善了高重合度人字齿轮的齿面偏载现象,降低了齿轮传动过程中的啮合冲击。对加工的人字齿轮在减振降噪试验台上进行带载试验,对比优化前后的噪音分贝值,进一步验证了该优化方法对人字齿轮副减振降噪具有一定作用。     

防空旅(团)战斗保障体系效能评估模型

防空旅(团)战斗保障体系的效能是形成良好防空作战能力的关键因素之一,结合防空旅(团)的实际情况,建立了防空旅(团)战斗保障体系的效能指标体系,应用AHP法(层次分析法)确立了各因素的权重,给定了防空旅(团)战斗保障体系效能的评价指标,采用模糊综合评判,建立了二级的评估模型,实现了对防空旅(团)战斗保障体系效能的量化评判模型,并通过实例分析证明了该方法的可行性。     

Transverse relaxation characteristic and stress relaxation model considering molecular chains of HTPB coating based on pre-strained thermal aging

In order to accurately describe the transverse relaxation characteristic and stress relaxation modulus of HTPB coating during pre-strain thermal aging process, a one month thermal aging test was carried out at 70 C with pre-strain of 0％, 3％, 6％ and 9％, respectively. The low-field 1H NMR and stress relaxation modulus tests were carried out for HTPB coating at different aging stages. The stress relaxation model considering the molecular chains was proposed according to the changes of crosslinking chain and dangling chain of HTPB coating during pre-strain aging. The results showed that with the increase of aging time, the decay rate of transverse relaxation curve became faster, the transverse relaxation time decreased, the value of combined parameter qMrl increased, the proportion of crosslinking chain decreased, while the proportion of dangling chain increased. Moreover, the stress relaxation modulus increased, the crosslinking network structure of HTPB coating became denser and the degree of cross-linking increased. At the initial aging stage, the pre-strain will destroy the crosslinking network structure of HTPB coating to a certain extent. With the increase of aging time, the effect of pre-strain will gradually weaken and the influence of aging on materials will gradually increase. The correlations between the stress relaxation model considering the molecular chains and the test results were more than 0.9950, which can accurately describe the stress relaxation modulus of HTPB coating during the pre-strain thermal aging process.     

激光防空武器系统作战效能研究

激光防空武器系统是一种新型的高技术多指标综合武器系统,其作战效能评估即是研究新型武器系统装备的主要依据,又是一件十分艰难的任务。依据WSEIAC提出的效能分析模型,建立了激光防空武器系统的ADC模型,对激光防空武器系统的作战效能作了研究,对其他武器的效能分析具有示范和借鉴作用。