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国家自然科学基金(10572022)

作品数:8 被引量:23H指数:3
相关作者:王天舒吕敬李俊峰岳宝增更多>>
相关机构:清华大学北京理工大学更多>>
发文基金:国家自然科学基金更多>>
相关领域:理学航空宇航科学技术更多>>

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充液挠性航天器俯仰运动分岔特性初步研究被引量:3
2008年
该文考虑了带弹性帆板与液体燃料的航天器做俯仰运动时刚-液-弹之间的相互耦合作用,采用已推导的刚-液-弹耦合系统非线性动力学方程组,应用多尺度法解析分析耦合系统的液体一阶主共振,利用奇异性理论对分岔方程进行分析,得到多种分岔模式,随后根据该文研究的耦合系统物理系数范围,确定只存在滞后点分岔,表现为幅频曲线软、硬特性的转换现象。
吕敬李俊峰王天舒岳宝增
关键词:俯仰多尺度分岔
充液柔性航天器非线性姿态动力学及再定向姿态机动
本文主要研究全充液柔性航天器大角度姿态机动中非线性姿态动力学及姿态再定向问题。采用Lagrange方法推导了液-柔耦合系统动力学方程并对系统进行了相空间动力学研究。由于能量耗散及柔性附件振动对系统产生扰动并由此引起混沌姿...
岳宝增
关键词:控制策略充液航天器
Dynamic response of liquid-filled rectangular tank with elastic appendages under pitching excitation被引量:2
2007年
Nonlinear dynamics of liquid-filled rectangular tank with elastic appendages are studied. Based on the assumption of ideal fluid, the coupling dynamic equations of rigid tank, elastic appendages and liquid fuel are derived using H-O principle. In the case of pitch excitation, the modified potential function and wave height function are introduced to describe the moving boundary of fluid, then Galerkin's method is used to discretize the dynamic equations into ordinary differential equations. The natural frequencics of the coupling system are formulated in liquid depth, the length of the tank, etc. The formulae are confirmed by numerical simulations, which also show that the effects of liquid and elastic appendages on the attitude angular of rigid.
吕敬李俊峰王天舒
关键词:PITCH
半充液柔性航天器姿态机动中同宿环分叉Melnikov判据
本文研究了带液体晃动和柔性附件的耦合航天器系统在液体燃料的耗散和柔性附件扭转振动的作用下,经历从最小惯量轴到最大惯量轴姿态转换机动中的混沌动力学行为。将液体晃动等效为球摆模型并由此建立了带柔性附件充液航天器多体耦合系统动...
岳宝增梁琼
关键词:充液航天器非线性
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Cassini贮腔中液体晃动频率特性研究
本文研究求解液体微幅自由晃动固有频率和振型的有限元数值计算方法,开发了针对Cassini贮箱中液体晃动特征值问题的计算程序。利用大型工程动力学分析软件ANSYS的前处理功能,实现了液体在不同充液比情况下的单元网格的划分,...
刘海燕岳宝增梁琼
关键词:固有频率振型有限元
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带自由液面液体非线性晃动的VOF方法
本文研究数值模拟含有自由液面的圆筒型贮腔内液体非线性晃动的液面波动情况。运用VOF方法追踪自由液面。介绍了VOF的主要原理,给出了左右壁面自由液面位置变化的时间历程以及自由液面的形状。
刘军岳宝增
关键词:VOF数值模拟
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In fluence of Sloshing on the Stability and Control for Spacecraft
<正>Fuel inside the spacecraft has the largest contribution of thetotal mass of spacecraft.The interaction of s...
Ahmad S
关键词:SLOSHING
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模式生成系统同宿环全局分岔问题研究
<正>仅限于研究一维情形。主要探索可激活模式中单脉冲及多脉冲解的失稳及其向复杂转换动力学的过渡机理。本工作的主要内容包括:在第2节给出了尺度化后的Gray-Scott模型并且简要分析了其稳态的稳定性。第3节叙述了本工作所...
岳宝增
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The least square particle finite element method for simulating large amplitude sloshing flows被引量:2
2008年
Large amplitude sloshing in tanks is simulated by the least square particle finite element method (LSPFEM) in this paper. The least square finite element method (LSFEM) is employed to spatially discrete the Navier-Stokes equations, and to avoid the stabilization issues due to the incompressibility condition for equal-order interpolation of the velocity and the pressure, as usually used in Galerkin method to satisfy the well-known LBB condition. The LSPFEM also uses the Lagrangian description to model the motion of nodes (particles). A mesh which connects these nodes is constructed by a triangulation algorithm to avoid the mesh distortion. A quasi a-shapes algorithm is used to identify the free surface boundary. The nodes are viewed as particles which can freely move and even separate from the main fluid domain. Finally this method is used to study the large amplitude sloshing evolution in two dimensional tanks. The results are compared with those obtained by Flow-3d with good agreement.
Bo Tang Junfeng Li Tianshu Wang
关键词:COLLAPSEIMPACT
Viscous flow with free surface motion by least square finite element method
2008年
A method for simulation of free surface problems is presented. Based on the viscous incompressible Navier-Stokes equations, space discretization of the flow is obtained by the least square finite element method. The time evolution is obtained by the finite difference method. Lagrangian description is used to track the free surface. The results are compared with the experimental dam break results, including water collapse in a 2D rectangular section and in a 3D cylinder section. A good agreement is achieved for the distance of surge front as well as the height of the residual column.
汤波李俊峰王天舒
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