期刊文献+
共找到3篇文章
< 1 >
每页显示 20 50 100
飞航导弹/涡扇发动机一体化设计-约束分析与任务分析 被引量:14
1
作者 陈玉春 刘振德 +2 位作者 史亚红 屠秋野 王晓东 《推进技术》 EI CAS CSCD 北大核心 2006年第3期216-220,共5页
利用飞机/涡扇发动机一体化设计的思路,建立了飞航导弹/涡扇发动机一体化设计的约束分析和任务分析模型并给出了算例和分析。简述了飞航导弹任务剖面、约束条件的给定、导弹的重量组成以及涡扇发动机模型。利用客机/货机升阻特性的预测... 利用飞机/涡扇发动机一体化设计的思路,建立了飞航导弹/涡扇发动机一体化设计的约束分析和任务分析模型并给出了算例和分析。简述了飞航导弹任务剖面、约束条件的给定、导弹的重量组成以及涡扇发动机模型。利用客机/货机升阻特性的预测方法对亚声速飞航导弹的升阻特性进行预测,并给出了合理的修正。利用经验的预测方法对亚声速飞航导弹的空重比进行预测。对飞航导弹的约束分析计算结果和任务分析计算结果表明,建立的飞航导弹/涡扇发动机一体化约束分析与任务分析模型是合理可行的,具有很好的工程实用价值。 展开更多
关键词 飞航式导弹 涡扇发动机 一体化设计 ^约束分析^+ ^任务分析^+
在线阅读 下载PDF
The Counting Problem of an Order N-group of Set 被引量:1
2
作者 WANGJing-zhou ZHANGHai-mo 《Chinese Quarterly Journal of Mathematics》 CSCD 2003年第3期283-285,共3页
In this paper, we discuss the counting prob lem of an order n-group of set (A 1,A 2,…,A n) which satisfies ∪ni=1A i={a 1,a 2,…,a m} and one of the following: (1) ∩ni=1A i=Φ; (2) ∩ni=1A i={b 1,b 2,…,b k};(3)... In this paper, we discuss the counting prob lem of an order n-group of set (A 1,A 2,…,A n) which satisfies ∪ni=1A i={a 1,a 2,…,a m} and one of the following: (1) ∩ni=1A i=Φ; (2) ∩ni=1A i={b 1,b 2,…,b k};(3) ∩ni=1A 1{b 1,b 2,…,b k}; (4) A i≠Φ (i=1,2,…,k). We solve these problems by element analytical meth od. 展开更多
关键词 an order n-group of set element analytical meth od COUNTING
在线阅读 下载PDF
Fatigue Analysis of Steel Catenary Risers Based on a Plasticity Model 被引量:1
3
作者 Yongqiang Dong Liping Sun 《Journal of Marine Science and Application》 CSCD 2015年第1期76-82,共7页
The most critical issue in the steel catenary riser design is to evaluate the fatigue damage in the touchdown zone accurately. Appropriate modeling of the riser-soil resistance in the touchdown zone can lead to signif... The most critical issue in the steel catenary riser design is to evaluate the fatigue damage in the touchdown zone accurately. Appropriate modeling of the riser-soil resistance in the touchdown zone can lead to significant cost reduction by optimizing design. This paper presents a plasticity model that can be applied to numerically simulate riser-soil interaction and evaluate dynamic responses and the fatigue damage of a steel catenary riser in the touchdown zone. Utilizing the model, numerous riser-soil elements are attached to the steel catenary riser finite elements, in which each simulates local foundation restraint along the riser touchdown zone. The riser-soil interaction plasticity model accounts for the behavior within an allowable combined loading surface. The model will be represented in this paper, allowing simple numerical implementation. More importantly, it can be incorporated within the structural analysis of a steel catenary riser with the finite element method. The applicability of the model is interpreted theoretically and the results are shown through application to an offshore 8.625 steel catenary riser example. The fatigue analysis results of the liner elastic riser-soil model are also shown. According to the comparison results of the two models, the fatigue life analysis results of the plasticity framework are reasonable and the horizontal effects of the riser-soil interaction can be included. 展开更多
关键词 steel catenary riser fatigue analysis riser-soil interaction plasticity model finite element method
在线阅读 下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部