整体壁板结构弯曲成形分析的等效塑性模型

大型整体壁板结构参数及成形工艺参数优化需要对壁板成形进行大量的非线性仿真计算,详细模型在计算时间和资源消耗方面难以接受,且不易收敛。通过弹塑性力学及回弹分析,基于应力和回弹后的变形等效,考虑了材料塑性变形强化效应,将整体壁板简化为某一虚拟材料的平板进行弹塑性弯曲等效分析。压弯和滚弯成形数值算例分析表明:在工程常用的弯曲半径范围内,变形计算误差在3.5%以内,应力误差在5%以内;等效模型大大减小了建模时间和资源,计算效率提高了70%以上,且计算易收敛;等效模型可以替代详细模型,为大型整体壁板结构参数及工艺参数优化、大型复杂形状壁板成形提供了快捷的分析方法。     

Hill区域内基于推广的Poincar映射的低能逃逸/捕捉轨道(英文)

给出了Hill区域内基于推广的Poincar映射的低能逃逸轨道的计算。文中的推广的Poincar映射需要在相空间中选取两个(而非一个)与流相截的面,即将包含某个天平动点的截面通过轨道来映射到近拱点的通道面上的,在数值上通过总变差减小的Runge-Kutta方法来实现两个相面之间的映射。捕捉轨道则可由Hill三体模型的对称性直接导出。最后,关于Rhea的二维、三维的逃逸和捕捉轨道的仿真结果验证了该方法的精度和鲁棒性。     

垂准仪校准的一个新方法

介绍了一种溯源于重力线的垂准仪校准方法;分析了＂顶杆式铅垂准线＂与＂平行光管式水平准线＂之间的联系与区别;基于顶杆式铅垂准线校准的几何模型,给出了天顶/底角的计算方法。     

Stifness modeling and analysis of a novel 4-DOF PKM for manufacturing large components

Faster response to orientation varying is one of the outstanding abilities of a parallel kinematic machine（PKM）.It enables such a system to act as a reconfgurable module employed to machine large components effciently.The stiffness formulation and analysis are the beforehand key tasks for its parameters design.A novel PKM with four degrees of freedom（DOFs）is proposed in this paper.The topology behind it is 2PUS-2PRS parallel mechanism.Its semianalytical stiffness model is frstly obtained,where the generalized Jacobian matrix of 2PUS-2PRS is formulated with the help of the screw theory and the stiffness coeffcients of complicated components are estimated by integrating fnite element analysis and numerical ftting.Under the help of the model,it is predicted that the property of system stiffness distributes within the given workspace,which features symmetry about a certain plane and is also verifed by performing fnite element analysis of the virtual prototype.Furthermore,key parameters affecting the system stiffness are identifed through sensitivity analysis.These provide insights for further optimization design of this PKM.     

基于AHP的高校毕业生就业质量评价模型构建

运用层次分析法(AHP),构建高校毕业生就业质量评价模型.实证结果表明,薪酬福利和个人发展指标在高校毕业生就业质量评价中所占权重较大;在二级指标中,劳动报酬、劳动合同和单位性质对高校毕业生就业质量评价的影响较大.     

基于划分检测模型的终端区异常轨迹检测方法

针对异常轨迹对轨迹聚类效果的影响以及给进离场程序管制适用性的量化分析提供分析数据的考虑,在结合数据挖掘中异常检测理论的基础上,利用划分检测框架及将距离和密度结合起来,设计了一种有效检测算法,运用到终端区飞行轨迹的异常检测当中,检测出飞行轨迹中的异常轨迹,从而改善轨迹的聚类效果。实例仿真结果表明：方法可以准确地检测出异常轨迹。     

拖靶系统挂机安装角度计算

拖靶安全释放是拖靶系统正常执行任务的前提,拖靶挂机安装角度的优劣直接影响着拖靶的安全释放.依据拖靶释放特性建立了拖靶系统动力学模型,提出了拖靶安全释放的条件,给出了拖靶挂机安装角度的计算方法;通过实例对方法的正确性进行了验证,其结果直接应用于某新型拖机改装试验中,取得了满意的效果.     

Generalized Kutta–Joukowski theorem for multi-vortex and multi-airfoil flow with vortex production——A general model

By using a special momentum approach and with the help of interchange between singularity velocity and induced flow velocity, we derive in a physical way explicit force formulas for twodimensional inviscid flow involving multiple bound and free vortices, multiple airfoils, and vortex production. These force formulas hold individually for each airfoil thus allowing for force decomposition, and the contributions to forces from singularities(such as bound and image vortices,sources, and doublets) and bodies out of an airfoil are related to their induced velocities at the locations of singularities inside this airfoil. The force contribution due to vortex production is related to the vortex production rate and the distance between each pair of vortices in production, thus frameindependent. The formulas are validated against a number of standard problems. These force formulas, which generalize the classic Kutta–Joukowski theorem(for a single bound vortex) and the recent generalized Lagally theorem(for problems without a bound vortex and vortex production) to more general cases, can be used to identify or understand the roles of outside vortices and bodies on the forces of the actual body, optimize arrangement of outside vortices and bodies for force enhancement or reduction, and derive analytical force formulas once the flow field is given or known.     

基于偏相关性分析的多设计要求快速优化设计方法

针对飞行器气动外形优化设计中的多设计点、多目标、多工程约束等多设计要求问题,提出了一种新优化设计方法———多设计要求快速优化设计方法。该方法立足于统计学中的偏相关性分析和线性回归理论,通过对设计变量和设计要求进行偏相关性分析,采用线性回归的方法构建设计变量与设计要求之间的转换模型,将多个设计要求转化为对设计变量的约束,从而简化了优化设计模型,减少了优化过程中调用求解器次数,提高了优化效率。利用该方法对RAE 2822和HSNLF(1)-0213翼型进行了多设计要求优化设计算例验证,并将优化结果与Pareto多目标优化方法结果进行对比,结果证明了本文方法的有效性和可靠性。     

基于Probit模型的航空差旅管理市场分析

研究分析企业和差旅管理公司的哪些因素会对差旅管理业务的选择产生影响,帮助差旅管理公司明确企业的差旅管理偏好,从而推动中国航空差旅管理市场的发展.针对航空差旅管理市场的现状,在对50家企业进行问卷调查后,通过Probit模型得出10个因素对企业选择差旅管理业务的影响程度,其中“现金流量”、“资金结算手段”、“增值服务种类”和“政策与系统的匹配度”4个因素具有显著性.最后,根据实证结果对企业和差旅管理公司提出相应的建议.