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131.
对于Poisson分布及正态分布,本文在其参数θ的先验一阶矩和二阶矩的部分信息已知的情况下,给出了θ的极小极大估计,同时也给出了最不利先验分布。  相似文献   
132.
战场备件模型探讨   总被引:1,自引:0,他引:1  
分析了战场条件下备件消耗的基本构成和特点,蛤出了备件消耗量模型及计算方法。根据两类备件消耗的不同特点,建立了备件携运量模型,并讨论了模型中参数的取值问题。  相似文献   
133.
从离子镀技术的基本原理、试验数据入手,探讨了采用多弧离子镀技术镀制大口径炮管的工作原理,并介绍了炮管镀膜设备的基本结构。试验结果表明,镀膜后的炮管,其表面硬度可提高6~9倍、耐磨性提高4倍以上,耐蚀性可达A级,防腐性能比其它方法高9倍以上。从而可有效地提高炮管的使用寿命和贮存可靠性。  相似文献   
134.
重庆市奉节县挖断村滑坡规模巨大,滑坡体长180~250m,滑坡体厚15~35m,剩余下滑力达5 337 kN/m,采用了前排全长后排埋入式的新型组合抗滑支挡技术,大大节省了工程投资。介绍了这种新型组合抗滑结构的设计方法,重点介绍了桩的长度计算、各桩承担滑坡推力计算、治理后的监测数据。工程竣工2年的监测数据表明滑坡变形趋于稳定,说明采用全长和埋入式组合抗滑桩治理该滑坡是有效的。  相似文献   
135.
坚持用科学发展观指导空军转型建设,必须牢牢把握“发展”这一主题,用新的发展思路实现空军更快更好发展;深入贯彻“统筹兼顾,协调发展”的方针,走出一条中国特色空军发展之路;始终坚持“以人为本”这个核心,以人才转型为先导带动空军转型建设全面发展。  相似文献   
136.
采用有限元计算方法研究了在4点弯曲载荷作用下,残余应力、涂层与基体的弹性模量比(简称弹性模量比)对涂层/基体材料界面能量释放率及其相角的影响。结果表明:能量释放率随着残余拉应力、弹性模量比的增大而增大;能量释放率中的相角也随着残余拉应力的增大而增大,但并不敏感,其随着弹性模量比的增大而减小。研究结果可为评价涂层/基体材料界面结合性能提供理论依据,有助于深化对涂层/基体材料界面结合性能的认识。  相似文献   
137.
The frequent occurrence of safety accidents during the calendering process is caused by the flammable and explosive properties of composite modified double-base (CMDB) propellant. Optimization of process parameters with the aid of fluid simulation technology could effectively ensure the safety of the calendering process. To improve the accuracy of the simulation results, material parameters and model structure were corrected based on actual conditions, and adaptive grid technology was applied in the local mesh refinement. In addition, the rheological behavior, motion trajectories and heat transfer mechanisms of CMDB propellant slurry were studied with different gaps, rotational rates and temperatures of two rollers. The results indicated that the refined mesh could significantly improve the contour clarity of boundaries and simulate the characteristics of CMDB propellant slurry reflux movement caused by the convergent flow near the outlet. Compared with the gap, the increased rotational rate of roller could promote the reflux movement and intensify the shear flow of slurry inside the flow region by viscous shear dragging. Meanwhile, under the synergistic effect of contact heat transfer as well as convective heat exchange, heat accumulated near the outlet and diffused along the reflux movement, which led to the countercurrent heat dissipation behavior of CMDB propellant slurry. The plasticizing mechanism of slurry and the safety of calendering under different conditions were explored, which provided theoretical guidance and reference data for the optimization of calendering process conditions. Based on the simulation results, the safety of the CMDB propellant calendering process could be significantly improved with a few tests conducted during a short research and development cycle.  相似文献   
138.
Currently,polarization visualization strategies are accomplished by mapping polarization information into a perceptually uniform color appearance model CAM02-UCS.However,the deviation of the CAM02-UCS space from the lightness prediction results in an inaccurate match between the polarization in-formation and the perceptual information.In this paper,we propose a novel polarization visualization strategy based on the perceptual uniform space Jzazbz.The polarization visualization be completed by placing the polarization information into the lightness Jz,colorfulness Cz and hue angle hz channels of the Jzazbz space.The experimental results show that the proposed method can significantly improve the lightness of the low irradiance and high polarization region,hence more polarization information can be sensed by human visual system.  相似文献   
139.
The aerodynamic characteristics are vital for short cylindrical Terminal Sensitive Bullets(TSB)with low aspect ratio,especially in terminal trajectory.Currently,there is little research in terms of the TSB and short cylinder with two free ends,and particularly in this trajectory,where the scanning angle β and roll angle α vary over a broad range between 0° and 180°.In this work,wind tunnel experiments are first conducted to learn the effects of Reynolds number and scanning angle on aerodynamic parameters for short cylinder with aspect ratio L/D = 1.Similar to infinite cylinder,for the short cylinder with two free ends,the drag crisis phenomenon still exists in the critical regime 1.7 × 105 ≤ Re ≤ 6.8 × 105.Then 3D simulations are performed to demonstrate the aerodynamic characteristics of short cylinder and TSB over a broad range of Re,L/D,α and β.The sensitivity analysis of time step and grid are presented as well.When β=0°,for short cylinder,the drag crisis phenomenon was also observed in the simulation,but not as obvious as in the wind tunnel test.In some attitudes,there is an obvious Kármán vortex in the wake of short cylinder and TSB.The correlation between time-averaged aerodynamic coefficients and L/D,Re,α&β is discussed.The vortex shedding frequency and shear layer behavior are obtained for quasi-steady and unsteady flow.Finally,the effect of end's shape on drag reduction and vortex shedding frequency is analyzed.  相似文献   
140.
In this study, the anti-penetration performance of polyurea/ASTM1405-steel composite plate subjected to high velocity projectile was analyzed. Two kinds of modified polyurea material (AMMT-053 and AMMT-055) were selected and a ballistic impact testing system including speed measuring target system and high-speed camera was designed. This experiment was conducted with a rifle and 5.8 mm projectile to explore the effects by the polyurea coating thickness, the polyurea coating position and the glass-fiber cloth on the anti-penetration performance of polyurea/ASTM1405-steel composite plate. The result showed that the effects of polyurea coating position were different between two types of polyurea, and that the effects of glass-fiber position were disparate between two types of polyurea as well. For AMMT-053 polyurea material, it was better to be on front face than on rear face; whereas for AMMT-055 pol-yurea, it was better to be on rear surface although the difference was very subtle. Additionally, formulas had been given to describe the relationship between the effectiveness of polyurea and the thickness of polyurea coating. In general, AMMT-055 had better anti-penetration performance than AMMT-053. Furthermore, five typical damage modes including self-healing, crack, local bulge, spallation and local fragmentation were defined and the failure mechanism was analyzed with the results of SHPB test. Additionally, the bonding strength played an important role in the anti-penetration performance of polyurea/steel composite plate.  相似文献   
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