基于Simulink的飞航式火箭助飞鱼雷空中弹道仿真

为研究飞航式火箭助飞鱼雷空中弹道参数设计问题,首先分析其空中运动过程,根据空中弹道的特点,建立了纵向运动方程组。采用MATLAB/Simulink软件建立了仿真模型,并就发射倾角、雷箭分离条件等对空中弹道的影响进行仿真计算。本文的研究成果对飞航式火箭助飞鱼雷空中弹道设计及作战效能研究有一定的参考价值。     

高速公路岩堆边坡仿真分析与评价研究

在分析宜巴高速公路三里花岩堆边坡基本特征及破坏机理的基础上,基于FLAC3D理论,建立了山区高速公路岩堆边坡三维仿真分析模型,在此基础上,考虑岩堆天然自重、降雨、地震和人类活动等荷载组合作用,模拟分析了岩堆边坡在不同工况条件下的变形破坏机理和稳定性,并对岩堆边坡的稳定状态进行了评价。     

多相感应电机磁势分析及仿真试验研究

分析了非正弦供电多相感应电机磁势,得出多相电机通过注入谐波可提高材料利用率的结论,通过试验和仿真验证了分析的正确性。     

A simulation approach for estimating value at risk in transportation infrastructure investment decisions

Traditional economic analysis techniques used in the assessment of Public Private Partnership (PPP) projects are based upon the assumption that future cash flows are fully deterministic in nature and are not designed to account for risks involved in the assessment of future returns. In reality, many of these infrastructure projects are associated with significant risks stemming from the lack of knowledge about future cost and benefit streams. The fundamental premise of the PPP concept is to efficiently allocate risks between the public and the private partner. The return based on deterministic analysis may not depict a true picture of future economic outcomes of a PPP project for the multiple agencies involved. This deficiency underscores the importance of risk-based economic analysis for such projects. In this paper, the authors present the concept of Value-at-Risk (VaR) as a measure of effectiveness (MOE) to assess the risk share for the public and private entity in a PPP project. Bootstrap simulation is used to generate the risk profile savings in vehicle operating cost, and in travel time resulting from demand-responsive traffic. The VaR for Internal Rate of Return (IRR) is determined for public and private entity. The methodology is applied to a case study involving such a joint venture in India, the Mumbai Pune Expressway/National Highway 4 (MPEW/NH4), and fiscal implications from the perspective of the public and the private entities are examined. A comparison between deterministic and risk based economic analysis for MPEW/NH4 is presented. Risk analysis provides insightful results on the economic and financial implications from each participant's viewpoint.     

Port authorities view state coastal management programs

Abstract

An estuarine sanctuary is a store of public values due to the ecological, cultural, recreational, aesthetic, historic, and economic services provided by the preserve. These values may be expected to increase over time because of (1) growth in the population demanding estuarine services, (2) growth in the willingness to pay for such services, and (3) growth in the actual quality and quantity of services which are provided by a protected natural system. Thus an estuarine sanctuary will be more valuable to future generations than to current generations. When weighing the cost and benefits of a preservation or development decision, a preservation decision which seems currently undesirable may in fact be socially beneficial when growth in the value of estuarine services is included.     

面向可再生能源利用的集装箱港口环境经济效益仿真

可再生能源具有环境友好、可循环利用等优点,综合利用可再生能源是绿色集装箱港口发展的必然趋势。应用系统仿真的方法量化港口装卸生产能源消耗量,结合环境经济效益计算方法定量分析可再生能源替代传统能源的环境经济效益。以某港区采用风力发电为例,对比分析集卡、岸桥和场桥能源替代后的环境效益与经济效益。     

试样厚度对船用钢疲劳裂纹扩展速率影响的试验

为研究试样厚度对船用钢疲劳裂纹扩展速率的影响,设计并实施两组不同厚度的紧凑拉伸试样进行疲劳裂纹扩展速率试验,同时建立了三维疲劳裂纹扩展有限元模型,分别基于线弹性理论和弹塑性理论对应力强度因子进行了计算,并分析了试样厚度对裂纹扩展速率的影响。试验与计算结果的综合分析表明：相同应力水平下,薄试样裂纹尖端的塑性区明显大于厚试样,且裂纹尖端应力强度因子值大于理论经验计算结果可达23.25%,因此,在材料裂纹扩展速率试验前,特别是试样厚度尺寸较小时,应充分考虑试样的厚度效应,参考基于弹塑性理论计算得到的应力强度因子结果,同时有必要针对当前试样及材料进行专门的裂纹扩展速率试验,以得到准确裂纹扩展参数结果。     

舰载直升机起降训练仿真系统设计方案

舰载直升机起降训练仿真系统是以计算机可视化技术及直升机、舰船运动数学模型为基础的复杂系统。提出了研制舰载直升机起降训练仿真系统的具体思路和设计方案,详细介绍了本系统中的海浪生成、舰船运动、直升机操纵等模块的数学模型及仿真实现。     

水中航行体绕流数值计算研究

水动力设计是水中航行体设计的重要组成部分.文章采用数值算法分别对水中航行体全湿和带空泡两种不同状态水下绕流问题进行了计算研究,并与风洞及水洞试验结果进行了对比.计算结果与试验值吻合较好,验证了数值算法的准确性.同时得到了水下绕流的某些运动规律,研究结果对工程设计起到了一定的帮助作用.     

双层壳体对水下爆炸作用的影响研究

针对目前设计部门感兴趣的双层壳体结构中外壳对水下爆炸作用的影响问题,用简单平面波理论对双层壳体结构的外板对冲击波的透射特性进行分析,给出透射冲击波的计算公式,与试验比较吻合良好.并详细介绍相关的双层平板的水下爆炸试验结果,表明双层壳体结构的外壳对水下爆炸作用的影响主要表现在高频部分,冲击波压力约减小20%,结构冲击加速度和应变响应减小约50%以上,内部流体的作用使对整体冲击响应速度略有增大.