基于激光推进的光船发射任务设计与参数优化分析

针对发射初始质量为100kg的光船到近地圆轨道的任务,研究了激光平均功率、激光大气传输特性、光船激光接收面面积、发动机比冲、发动机能量转化效率等参数之间的相互关系及光船飞行任务的优化问题。针对激光发射光船的具体要求,由功率估算公式计算出激光平均功率,从激光作用范围估算出光船的激光接收面的最小面积;基于光船飞行动力学模型,结合估算的参数,应用序列二次规划方法优化计算出光船飞行的最优弹道。计算结果表明,光船入轨质量可达到35.5kg,最优比冲为8140m/s。     

切尔诺贝利核事故救援对我国核电消防部队建设的启示

介绍了切尔诺贝利核事故消防部队救援的基本情况以及经验和教训,并针对我国目前核电消防的现状,结合切尔诺贝利核事故救援的经验和教训,就我国核电消防安全和队伍建设提出了建议和意见。     

基于动量流量法对喷水推进系统推力的CFD计算

采用结构化网格与非结构化网格相结合的方式划分了喷水推进系统的流场区域,采用稳态多参考系方法进行了数值计算。在此基础上,定义并求解一用户自定义标量函数标记整个流场,并根据标记结果将被喷水推进器吸入的流体与其它流体区分开。在后处理过程采用标量函数的等值面来确定喷水推进系统控制体上的流管分界面和进流面。利用数值计算所得的速度场对喷水推进系统喷口和进流面上的动量流量变化率进行计算,间接地得到喷水推进系统的推力。计算结果表明,采用CFD手段计算和分析喷水推进系统包括推力在内的各项性能指标是可行的。     

混合电推进能源管理系统模糊逻辑控制

针对混合电推进能源管理方法开展研究,设计了一种基于模糊逻辑控制的混合电推进能源管理系统。通过设置垂直起降飞行器的功率要求、内燃机-发电机输出功率和储能电池荷电状态的模糊隶属度函数,动态最优分配发电机与储能电池的功率输出,从而提升系统的燃油经济性与飞行器的航程。结合模型设置,对100 kg级的垂直起降转平飞的飞行器能源系统变化进行仿真计算,验证了能源控制算法的可行性。结果表明：基于模糊逻辑控制的能源管理方法,在总时长约为1.2 h的飞行过程中,内燃机约有1 h的时间工作在比油耗最低的区域,从而提升了混合电推进系统的能量利用效率。研究为后续混合电推进系统的能源高效控制与管理提供了设计思路和分析方法。     

用三维非线性Langevin方程计算裂变碎片质量分布

采用扩散模型,利用｛ｃ,ｈ,ａ｝三参数描述核形状,建立了三维非线性Ｌａｎｇｅｖｉｎ方程。用Ｍ—Ｃ方法模拟了核的形变运动,计算了处于高激发态的~（１９８）Ｈｇ,~（２１０）Ｐｏ和~（１８５）Ｒｅ核的裂变碎片质量分布。给出了裂变碎片的平均质量、均方差及最可几值等物理量。计算结果与实验值定性一致。     

Let’s make a (nuclear) deal: Bargaining,credibility, and the third offset strategy

An institutional perspective on nuclear deterrence cooperation within alliances has the potential to fundamentally reorient how we think about analyzing nuclear and deterrence decision-making between nuclear patrons and non-nuclear clients. It comes at a time when the presidency of Donald Trump is sure to test many of the core claims and assumptions in security studies, especially relating to bargaining and credibility within alliances. This article surveys questions that will be core to the research agenda involving alliance institutions and nuclear weapons during the Trump presidency and beyond.     

‘A Sledgehammer to Crack a Nut’? Naval Gunfire Support During the Malayan Emergency

The utility of naval gunfire support (NGS) during the Malayan Emergency has been the subject of significant scrutiny. While the limitations of NGS were demonstrated in Malaya, it also has proven to be extremely useful under certain circumstances. The circumstances in which NGS has proven effective during earlier and later insurgencies have generally reflected those of the Malayan Emergency. Recent operations in Afghanistan and Iraq have been less conducive to the application of maritime power, but they did not denote the end of the naval role or the potential usefulness of NGS in counterinsurgency operations. NGS is an unheralded capability, but, aside from the historical significance, it remains relevant in the contemporary era under the right conditions.     

Enhancing Political Cohesion in NATO during the 1950s or: How it Learned to Stop Worrying and Love the (Tactical) Bomb

This article argues that the perceived need by NATO to nurture political cohesion within the Alliance during the 1950s resulted in the adoption of strategic concepts that were out-of-step with the military environment in which it was operating. It maintains that the Alliance acquiesced to American leadership on nuclear issues which led to the development of tactical nuclear capabilities at the expense of conventional war-fighting capabilities for the defence of the European Central Front. This resulted in a strategic concept that enhanced political cohesion but was militarily unviable.     

喷水推进装置及其在舰艇上的应用

船舶喷水推进装置具有推进效率高、噪音小、操作性能好以及适合浅水航行等特点,其军事价值将越来越受到世界各国海军的重视.分析了喷水推进装置的优、缺点,简要介绍了其基本原理和结构,并总结了其在潜艇和水面舰艇上的应用,对其今后的应用与发展趋势作了简要分析.     

并联TBCC动力对高超声速飞行器性能的影响

针对马赫数为6的一级高超声速巡航飞行器的动力需求,提出涡轮/亚燃冲压/双模态超燃冲压组合动力（T/RJ/DMSJ）和射流预冷涡轮/亚燃冲压/双模态超燃冲压组合动力(PCT/RJ/DMSJ)两种方案。在给定的飞行任务下,分析起飞推重比分别为0.8和1.0时,飞行器完成任务时的航程和飞行时间,并对比了PCT/RJ/DMSJ在两种工作模态下的性能。研究结果表明：在相同的起飞推重比下,两种组合动力方案的航程和飞行时间相差不大。当起飞推重比为0.8时,采用PCT/RJ/DMSJ组合动力方案比T/RJ/DMSJ组合动力方案的航程高出3.6%,飞行时间高出3.8%;当起飞推重比为1.0时,PCT/RJ/DMSJ的航程和飞行时间比T/RJ/DMSJ的分别高出4.6%和4.8%。在小推重比下,跨声速段的燃料消耗和飞行时间占整个加速爬升段的比例较大,随着推重比的增加,这个比例减小,巡航可用的燃料比例增大,巡航距离增加,提高起飞推重比可以提高超声速飞行器的航程并缩短飞行时间。