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51.
潜艇纯方位接敌跟踪航路优化方法探讨   总被引:2,自引:0,他引:2  
潜艇利用纯方位定位跟踪系统对目标进行定位跟踪时 ,目标位置线在优化潜艇的接敌跟踪航路中具有重要的作用。通过研究目标位置点与目标位置线和目标方位之间的关系 ,构造出一个优化潜艇接敌跟踪航路模型  相似文献   
52.
鹤管气阻与泵汽蚀所指的对象不同,但两者具有相同的物理意义,都是指当液体介质的绝对压力小于其实时饱和蒸气压时所体现的物理现象。阐述了鹤管气阻的原因及目前解决的措施,分析了离心泵汽蚀方程的物理意义。根据能量平衡方程,推导出吸入系统管道不发生气阻的安装高度方程,并与泵不发生汽蚀的安装高度方程进行了对比分析。最后得出结论,要保证离心泵正常工作,必须同时满足吸入系统工艺管道安装高度要求以及泵安装高度要求。  相似文献   
53.
单端起爆螺旋形爆炸磁通压缩发电机的等效电路模型   总被引:3,自引:0,他引:3  
从磁通守恒原理出发 ,通过建立单端起爆螺旋形爆炸磁通压缩发电机 (EMCG)的等效电路模型 ,详细地分析了这种发电机在压缩运行过程中各有关的物理量及其相互关系 ,为进行数值模拟和装置设计提供了有用的参考。  相似文献   
54.
Statistical estimation plays an important role in locating a target in space, a task that has important applications in many areas. However, theoretical measures on the quality of various estimators reported in the literature have been difficult to obtain because of mathematical complications. As a result, choice of estimator in practice has been largely arbitrary. In this paper, we present a systematic study on major target estimators reported in the literature. Focus is on comparisons between the traditional angle method, the line method, and a recently developed line-to-point transformation method. Insights gained from the study directly lead to the development of a novel two-stage angle method that not only produces highly accurate target estimation among all known estimators but is also computationally efficient. © 1998 John Wiley & Sons, Inc. Naval Research Logistics 45: 353–364, 1998  相似文献   
55.
本文导出了一种较为普遍的传热规律 q∝△(T~n)时内可逆卡诺热泵的最佳供热系数、利润率关系,并藉此讨论了几种传热规律时内可逆卡诺热泵的有限时间(火用)经济最优性能,得到了一些新的普适结果。  相似文献   
56.
本文导出工质与三个热源间的传热系数分别为。α、β和γ,传热规律为q~∝△(T~(-1))时,内可逆三热源热泵的最佳供热系数ψ与供热率Π间的关系:ψ<1时,Π=K_1ψ[T_p(T_H-T_ο)-T_H(T_p-Tο)ψ]/[T_HT_pT_ο(1-△_1ψ)~2];ψ>1时,Π=K_2ψ[T_p(T_H-T_ο)-T_H(T_P-T_ο)ψ]/[T_HT_pT_ο(△_2-ψ)~2];式中,K_1=αγ/(α~(1/2)+γ~(1/2))~2,K_2=βγ/(β~(1/2)+γ~(1/2))~2,△_1=(α/β)~(1/2)(β~(1/2)-r~(1/2)/(α~(1/2)+γ~(1/2)),△_2=(β/α)~(1/2)(α~(1/2)-γ~(1/2))/(β~(1/2)+γ~(1/2))。由此可得许多有用的关系。  相似文献   
57.
《防务技术》2019,15(4):645-654
In order to study influence of tongue clearance on the hydraulic performance of double support vortex pump, three dimensional flow model with symmetric variable size tongue clearance was established by changing section parameter of tongue clearance, and applied to numerically simulate the steady inner flow in a vortex pump based on fixed working conditions and impeller through ANSYS FLUENT. The numerical results show the influence of tongue channel with two sections (non-uniform and uniform sections) on flow field characteristics in vortex pump. Firstly, the variation of tongue channel section changes the vortex structure distribution in circumferential flow channel. Specifically the spiral forward vortex structure in the circumferential direction shifts to large radius side with increasing tongue width. Secondly, the circumferential velocity gradient and axial pressure gradient both diminish with the increase of the tongue section, and the inlet/outlet pressure difference and velocity distribution also reduce with increasing tongue channel section. Finally, for vortex pump with non-uniform section of tongue channel, the head diminishes and the efficiency remains constant approximately with the increase of the tongue width, while the head and the efficiency both diminish for uniform section of tongue channel.  相似文献   
58.
In this article, we study a queueing system serving multiple classes of customers. Each class has a finite‐calling population. The customers are served according to the preemptive‐resume priority policy. We assume general distributions for the service times. For each priority class, we derive the steady‐state system size distributions at departure/arrival and arbitrary time epochs. We introduce the residual augmented process completion times conditioned on the number of customers in the system to obtain the system time distribution. We then extend the model by assuming that the server is subject to operation‐independent failures upon which a repair process with random duration starts immediately. We also demonstrate how setup times, which may be required before resuming interrupted service or picking up a new customer, can be incorporated in the model. © 2013 Wiley Periodicals, Inc. Naval Research Logistics, 2013  相似文献   
59.
基于辅助制导的无人飞行器多航迹规划是现今航迹规划的主流研究方向之一。飞行器规划空间广,规划过程耗时长,如何提高航迹规划的速度是一个急待解决的问题。因此,提出了一种在预处理过程中生成的、满足战场环境和基于辅助制导无人飞行器飞行特性的有向航迹网络图。该网络图适用于基于辅助制导的无人飞行器多航迹快速规划,使用数据库存储和管理,具有整体数据结构化、易扩充、占用内存资源小、可大大缩短规划时间等优点。  相似文献   
60.
Abstract

This paper explains and assesses the UK experience with determining prices and profitability for non-competitive defence contracts. Three periods are considered, namely pre-1968, the 1968 Profit Formula Agreement and the changes introduced in 2014. Two cases of ‘excessive’ profits were major determinants of the 1968 Profit Formula Agreement; but continued dissatisfaction with the 1968 Agreement led to changes in 2014. The historical overview of UK experience provides a basis for understanding current UK policy and offers insights for other countries facing similar policy challenges. A critique is presented of UK policy on single source pricing and profitability.  相似文献   
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