钉载作用下层板多孔过盈配合分析

本文利用各向异性体平面弹性理论中的复势方法,以Faber级数为工具,导出层板多孔/弹性核过盈配合在钉载作用下的级数解。     

数据链试飞电波传播衰减计算

数据链作用距离的试飞结果受试验区电波传播衰减影响很大,需要对其进行精确计算,为分析试飞结果提供支持.Fock级数法是计算电波衰减的一种精确方法,本文详细讨论了应用该方法求解试验区电波传播衰减的工程计算问题.     

基于状态空间的流固耦合传热的分析

研究了半无限大管道中定常热物性牛顿流体的处于热充分发展状态的一维的流固耦合瞬时强制对流换热，基于状态空间描述法，发展了上述场合的较简单的封闭解法，得到了三维条件下以下两种情况的分析解：(1)恒稳态；(2)瞬态早期阶段。并对n个流体、m个固体串联的管道中一维的耦合热交换问题给出了一般解法，借助于MATLAB强大的矩阵处理功能，本解法更为快速有效。最后，通过实验测试验证了分析解的结果。     

Distributed online mission planning for multi-player space pursuit and evasion

There are three important roles in evasion conflict: pursuer, target and defender. Pur-suers’ mission is to access targets;targets’ mission is to escape from pursuers’ capture;defenders’ mission is to intercept pursuers who are potentially dangerous to targets. In this paper, a distributed online mission plan (DOMP) algorithm for pursuers is proposed based on fuzzy evaluation and Nash equilibrium. First, an integrated effectiveness evaluation model is given. Then, the details of collaborative mission planning which includes the co-optimization of task distributing, trajectory and corresponding maneuvering scheme are presented. Finally, the convergence and steadiness of DOMP are discussed with simulation results. Compared with centralized mission planning, DOMP is more robust and can greatly improve the effectiveness of pursuing. It can be applied to dynamic scenario due to its distributed architecture.     

一类有正阻尼的强非线性振动问题的近似解

用线化法,权残法和插值摄动法相结合的方法求得了一类有正阻尼的强非线性振动问题的近似瞬态解,精度好。     

应用摄动法确定飞机的模态特性

应用摄动法将飞机四阶线化方程降为二阶方程，导出确定飞机纵向长，短周期模态和模航向滚转，螺旋，荷兰滚模态近似解析解。     

固溶制度对7050铝合金微观组织和腐蚀性能的影响

采用光学显微镜(OA)、扫描电镜(SEM)、透射电镜(TEM)等手段和电化学、浸蚀、慢应变速率拉伸(SSRT)等测试方法,研究不同固溶热处理制度对7050铝合金板材微观组织和腐蚀性能的影响。结果表明:单级固溶将η(MgZn2)相完全溶入Al基体中,而S(Al2CuMg)相仍然大量存在,固溶度低,时效后晶内析出密度低;双级固溶使S相部分溶解,合金晶粒长大,再结晶分数高;逐级固溶使η和S相完全溶解,合金充分回复,时效后晶内析出密度高,再结晶分数低;不同固溶+T6时效态合金的抗应力腐蚀性能从大到小依次为逐级固溶>双级固溶>单级固溶。     

新淬火状态铝合金板的成形极限

论述了硬铝合金成形工艺中应变路径、固溶热处理和时效过程对成形极限的影响,由试验得到了单向拉伸预应变和固溶热处理后时效过程中的成形极限图FLD(Forming Limit Diagram),重点研究了固溶热处理后时效过程中成形极限的变化,并得到了铝合金在时效过程中的成形极限应力图FLSD(Forming Limit Stress Diagram).结果表明,原始退火状态材料的成形极限高于新淬火状态材料的成形极限,且新淬火状态材料的成形极限随时效时间增加而降低,原因主要在于固溶热处理过程中材料组织状态的变化和应变硬化指数n在时效过程中的降低;成形极限应变的降低导致成形极限应力也随时效时间增加而降低.      

可行域为有限集的多目标规划的一种解法

本文对可行域为有限集的多目标规划，给出了求其ｐａｒｅｔｏ有效解和弱ｐｅｒｅｔｏ有效解的一种解法。     

Symmetric Mach reflection configuration with asymmetric unsteady solution

Symmetric Mach reflection in steady supersonic flow has been usually studied by solving a half-plane problem with the symmetric line treated as reflecting surface, thus losing the opportunity to discover antisymmetric flow structures. Here in this paper we treat this problem as an entire-plane problem. Using an unsteady numerical approach, we find that the two sliplines exhibit antisymmetric unsteadiness if the Mach stem height is small while the flow remains symmetric if the Mach stem height is large. The mechanism by which disturbance, generated in the downstream of the flow duct between the two sliplines, propagates upstream is identified and it is also shown that the interaction between the transmitted expansion waves and the sliplines increases the amplitude of the unstable modes. The present study suggests a new type of compressible jet that deserves further studies.