期刊文献+
共找到7篇文章
< 1 >
每页显示 20 50 100
基于虚载荷变量的无网格法形状优化的研究
1
作者 邱爱红 龚曙光 +1 位作者 黄云清 聂松辉 《工程力学》 EI CSCD 北大核心 2007年第9期26-30,36,共6页
将选择施加在"虚结构"控制点上的虚载荷作为形状优化的设计变量,并将它与无网格Galerkin法相结合来开展结构形状优化研究,采用罚函数法来施加边界条件,通过直接微分法建立了结构形状优化的离散型灵敏度分析算法,利用无网格法... 将选择施加在"虚结构"控制点上的虚载荷作为形状优化的设计变量,并将它与无网格Galerkin法相结合来开展结构形状优化研究,采用罚函数法来施加边界条件,通过直接微分法建立了结构形状优化的离散型灵敏度分析算法,利用无网格法研究了节点坐标关于设计变量导数的计算。所提出的算法简单明了,它不仅解决了网格的畸变问题,而且简化了优化模型和迭代流程,并可使结构的受力特性得到进一步的改善。最后用2个工程实例验证了所建立的算法,并得到了形状优化结果。 展开更多
关键词 形状优化 无网格GALERKIN法 灵敏度分析 载荷变量 罚函数法
下载PDF
多工况应力下船舶多载荷作用下连续体结构拓扑优化 被引量:1
2
作者 赵宏旺 《舰船科学技术》 北大核心 2019年第6期1-3,共3页
在多载荷作用下,为使船舶连续体结构的拓扑算子与工况应力条件保持统一变化趋势,提出多工况应力下的新型船舶连续体结构拓扑优化方法。受限选取适宜的船舶载荷变量,再根据连续体结构的单元密度过滤条件,设置多载荷拓扑空洞值,最后在计... 在多载荷作用下,为使船舶连续体结构的拓扑算子与工况应力条件保持统一变化趋势,提出多工况应力下的新型船舶连续体结构拓扑优化方法。受限选取适宜的船舶载荷变量,再根据连续体结构的单元密度过滤条件,设置多载荷拓扑空洞值,最后在计算船舶连续体结构刚度的基础上,对整体优化流程进行完善,完成多工况应力下船舶多载荷作用下连续体结构拓扑优化方法的搭建。对比实验结果表明,在多载荷作用下,应用新型优化方法后,船舶连续体拓扑结构与工况应力条件间的最大影响参量可达1.24,远超理想最大影响参量0.66,使船舶连续体结构的拓扑算子与工况应力条件达到高度统一状态。 展开更多
关键词 多工况应力 载荷作用 结构拓扑 载荷变量 单元密度
下载PDF
飞机颠簸的预报 被引量:2
3
作者 郭虎道 俞飞 《河南气象》 2002年第2期26-27,共2页
通过对经验预报、理查逊数 (Ri)预报、载荷因数变量方程预报等 3种颠簸预报方法的讨论 ,得出了不同的天气系统及环境、风的水平与垂直切变、大气层结、温度的水平与垂直梯度、温度的局地变化等多个气象因子与颠簸的关系 。
关键词 飞机颠簸 大气湍流 理查逊数 载荷因数变量方程 预报指标 据动气流
下载PDF
飞机颠簸的预报 被引量:3
4
作者 陈华利 《四川气象》 1999年第3期32-33,共2页
从飞机动力学方程出发,得出了载荷系数变量方程。分析了产生颠簸的物理本质,讨论了颠簸强度与气象因子之间的关系避开了预报颠簸只注重天气形势而忽略其物理过程的常规预报方法,提出了预报飞机颠簸的几个适用可行的指标,可从进一步... 从飞机动力学方程出发,得出了载荷系数变量方程。分析了产生颠簸的物理本质,讨论了颠簸强度与气象因子之间的关系避开了预报颠簸只注重天气形势而忽略其物理过程的常规预报方法,提出了预报飞机颠簸的几个适用可行的指标,可从进一步提高对颠簸的预报能力。 展开更多
关键词 升力 载荷系数变量 飞机 颠簸预报 气象因子
下载PDF
Fuel load and flight ranges of blackcaps Sylvia atricapilla in northern Iberia during autumn and spring migrations
5
作者 Juan ARIZAGA Emilio BARBA 《Current Zoology》 SCIE CAS CSCD 北大核心 2009年第6期401-410,共10页
Fuel accumulation, mainly as fatty acids, is one of the main characteristics of migratory, birds. Studying to what extent each population or species manages fuel load and how it varies along routes of migration or bet... Fuel accumulation, mainly as fatty acids, is one of the main characteristics of migratory, birds. Studying to what extent each population or species manages fuel load and how it varies along routes of migration or between seasons (autumn and spring migrations) is crucial to our understanding of bird migration strategies. Our aim here was to analyse whether migratory blackcaps Sylvia atrieapilla passing through northern Iberia differ in their mean fuel loads, rate of fuel accumulation and ' potential' flight ranges between migration seasons. Blackcaps were mist netted for 4 h-periods beginning at dawn from 16 September to 15 November 2003 - 2005, and from 1 March to 30 April 2004 - 2006 in a European Atlantic hedgerow at Loza, northern Iberia. Both fuel load and fuel deposition rate (this latter assessed with difference in body mass of within-season recaptured individuals) were higher in autumn than in spring. Possible hypotheses explaining these results could be seasonal-associated variations in food availability (likely lower during spring than during autumn), the fact that a fraction of the migrants captured in spring could breed close to the study area and different selective pressures for breeding and wintering 展开更多
关键词 BLACKCAP Srlvia atricapilla Fuel load lberia Migration STOPOVER
下载PDF
Prediction of Hub Corner Stall Characteristics of a Highly Loaded Low Speed Single Stage Fan 被引量:4
6
作者 S. Farhan Ali Hashmi 《Journal of Thermal Science》 SCIE EI CAS CSCD 2011年第2期106-114,共9页
In this paper a numerical investigation has been presented on the stall mechanism of a highly loaded Single Stage Low Speed Fan designed for the research test facility to be installed at North Western Polytechnic Univ... In this paper a numerical investigation has been presented on the stall mechanism of a highly loaded Single Stage Low Speed Fan designed for the research test facility to be installed at North Western Polytechnic University (NWPU) Xi’an, China. The results presented are for the design point, near stall and just stall operating conditions at design speed. Design point studies have been found to be an indicative of stall area. Unsteady method of domain scaling has been used to compute the results at near stall and just stall conditions. It has been found that unlike the conventional tip leakage flow of the rotor, stator hub section is mainly responsible for the stall of the fan. The flow mechanism has been discussed with correlation to the design variables and previous investigations. Commercial CFD code NUMECA FINE/Turbo has been used for computations; results have been compared with results obtained from commercial CFD code ANSYS-CFX. The loss prediction of latter code is conservative than the former. The stall mechanism predicted by both codes is analogous. 展开更多
关键词 Low stage reaction STALL Rotor hub corner separation Stator hub corner separation 3D flow separation
原文传递
Interval design point method for calculating the reliability of structural systems 被引量:2
7
作者 NI Zao QIU ZhiPing 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2013年第11期2151-2161,共11页
The evaluation of reliability for structural system is important in engineering practices.In this paper,by combining the design point method,JC method,interval analysis theory,and increment load method,we propose a ne... The evaluation of reliability for structural system is important in engineering practices.In this paper,by combining the design point method,JC method,interval analysis theory,and increment load method,we propose a new interval design point method for the reliability of structural systems in which the distribution parameters of random variables are described as interval variables.The proposed method may provide exact probabilistic interval reliability of structures whose random variables can have either a normal or abnormal distribution form.At last,we show the feasibility of the proposed approach through a typical example. 展开更多
关键词 PROBABILITY design point method interval analysis probabilistic interval reliability parameters UNCERTAINTY
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部