Involving the elephant: technical isolation and the role of India in a possible solution to the Iranian nuclear crisis

Apart from North Korea, no state's nuclear program in the twenty-first century has raised more concern to international security than Iran's. While Iran insists that its nuclear program is strictly for civilian purpose in line with Article IV of non-proliferation treaty, the USA and its allies insist that Iran has military intentions and called for sanctions. The failure of sanctions to deter Iran from its nuclear agenda had made many scholars and policy-makers call for a preemptive attack on Iranian nuclear facilities. Situated within this debate, this paper positions itself as an antagonist to the preemptive airstrike option and argues that involving India in a possible nuclear “iron curtain” against Iran – a move known as technical isolation – remains the best option to the current nuclear crises.     

单兵系统数据模型

讨论了单兵系统的体系结构和信息要素,并结合单兵系统在联合作战中的应用例子,对其业务过程和信息流进行初步分析。然后通过IDEF1X方法,设计单兵系统基于关系数据库的数据模型。最后讨论了模型的规范化问题,并给出检验数据模型的方法。     

PCA和ICA的舰船尾流后向散射光信号检测

水体的后向散射光信号是舰船尾流后向散射光信号检测的常见干扰,由于其在频域十分接近且信号强度大于尾流信号,因此严重影响了有用信号的提取。针对这一问题,提出了一种基于主成分分析(PCA)和独立成分分析(ICA)相结合的尾流散射光信号检测方法。首先使用主成分分析对采集的散射光信号进行降维,去除冗余成分,之后使用基于负熵的F astICA算法对数据进行处理,分离了水体和舰船尾流的散射光信号,通过实验验证了该算法的有效性。     

水下航行器头部流噪声数值仿真与实验

选取头部线型,对航行器头部基于RNG k-ε湍流模型及FW-H声学模型进行流噪声模拟,然后对3种头部线型的航行器在不同速度下分别进行水洞实验。通过对比分析数值仿真与实验结果发现,航行器头部流噪声随着频率的增大而逐渐减小,随着速度的增大而增大。在相同速度下,与头部线型2、头部线型3相比,头部线型1流噪声较小,具有更好的降噪作用。所采用的计算方法可以比较准确地模拟航行器头部流噪声情况。     

切向空气气流对激光辐照碳纤维复合材料的影响

实验研究了靶材表面存在和不存在切向空气气流时,975nm连续激光对碳纤维增强树脂基复合材料的辐照效应,发现切向气流的加载有利于激光对碳纤维复合材料的破坏.从理论上对激光辐照下碳纤维复合材料的破坏机理进行了初步分析,基于碳的氧化特性和氧化反应机理,推导了碳纤维的氧化速率方程.采用改进的光滑粒子方法,对激光辐照下复合材料树...     

如何估计软件的MTBF

软件剩余初始故障个数No、平均无故障时间MTBF、故障暴露率λ和软件运行的成功率θ等是衡量软件可靠性的重要参数.其中对高可靠性软件(包括军用软件等)MTBF是最重要的.传统的MTBF计算方法有2种一是计算发生故障的平均时间间隔二是通过软件可靠性模型进行估计.前者代价较大,后者不太准确.本文从软件的失败率入手研究软件的MTBF,这是一个比较贴近实际的方法.     

后方油库整体生存概率分析计算

针对我军后方油库特点,探讨了油库整体生存概率计算的基本思路和方法,分析了各类分项目标生存概率的计算方法,采用层次分析对后方油库各分项目标权值进行了详细分析计算,可为后方油库伪装防护效能评估提供依据。     

数值模拟类升力体外形高超声速粘性绕流

采用空间二阶精度的交替方向隐式分解的NND格式求解完全气体假定下的非定常薄层近似Navier Stokes方程 ,并采用抛物化的椭圆型方程生成复杂带翼外形的空间网格。最后给出了类升力体外形在M∞ =8 0 ,α =2 0°下的流场计算结果。     

Optimal (τ, T) opportunistic maintenance of a k‐out‐of‐n:G system with imperfect PM and partial failure

The opportunistic maintenance of a k‐out‐of‐n:G system with imperfect preventive maintenance (PM) is studied in this paper, where partial failure is allowed. In many applications, the optimal maintenance actions for one component often depend on the states of the other components and system reliability requirements. Two new (τ, T) opportunistic maintenance models with the consideration of reliability requirements are proposed. In these two models, only minimal repairs are performed on failed components before time τ and the corrective maintenance (CM) of all failed components are combined with PM of all functioning but deteriorated components after τ; if the system survives to time T without perfect maintenance, it will be subject to PM at time T. Considering maintenance time, asymptotic system cost rate and availability are derived. The results obtained generalize and unify some previous research in this area. Application to aircraft engine maintenance is presented. © 2000 John Wiley & Sons;, Inc. Naval Research Logistics 47: 223–239, 2000     

线导鱼雷导引弹道的动力学分析

通过线导鱼雷常用导引方法—三点法、前置角法导引弹道的动力学分析 ,推导出不同方法下鱼雷旋回速率的解析表达式 ,并通过数字仿真对鱼雷线导导引弹道动力学特性进行探讨 ,明确了线导鱼雷导引弹道特性与导引方法之间的关系 .