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炮身沿摇架大位移后坐系统的时空有限元建模方法研究
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摘要
本文以某国防项目为研究背景,利用理论分析、数值计算和实验测试相结合的方法,按照循序渐进的思路对炮身沿摇架大位移后坐系统的时空有限元建模理论与方法进行探讨研究。
     对时空有限元法的基本建模理论进行了讨论分析,结合经典的移动惯性载荷作用下弦的振动问题,编制了求解结构动力学问题的时空有限元算法程序,基于经典算例,将计算结果与精确解、Newmark法、Wilson-θ法、中心差分法等进行比较分析,验证该算法的精度和稳定性。
     建立了移动力/移动质量作用下的简支梁和悬臂梁的时变力学模型,在传统有限元质量矩阵和刚度矩阵的基础上,利用迭代格式对位移和速度进行更新,推导出每个时间步上的时空质量矩阵和刚度矩阵,以简支梁和悬臂梁为例,计算移动力/移动质量以一定的速度匀速通过时的动力响应,并与精确解、Newmark法、Wilson-θ法等进行分析对比,进一步验证时空有限元法的有效性。
     建立了炮身沿摇架大位移后坐的时变动力学模型,给出了相应的时空有限元数值算法,将摇架简化成悬臂梁,炮身分别用移动刚体、移动簧载质量、移动簧载刚体、移动梁等来模拟,利用时空有限元法进行时域和空间域的离散,获得了时变动力学方程组,通过数值计算得到了炮身沿摇架大位移后坐的动力响应。
     对炮身沿摇架大位移后坐的振动特性进行了测试研究,将理论计算与实验结果进行对比分析,验证了理论建模的正确性。
     本文取得的炮身沿摇架大位移后坐时变系统的时空有限元数值计算初步成果对深入开展火炮大位移时变动力学设计理论研究具有一定的借鉴作用。
Under the background of a National Defense Project, this thesis is concerned with space-time finite element modeling theory and method for a canon barrel with large displacement by combination of theoretical analysis, numeric calculation and experiment.
     Basic modeling theory on space-time finite element method is analysised. Combining with the classical case of string vibration under moving inertial load, the algorithm program for solving structural dynamic problems is compiled. Based on classical examples, the results are compared with the exact solution, the Newmark method, Wilson-θmethod and Central difference method, which verifies the accuracy and stability of this algorithm.
     A time-varying mechanical model of simply supported beam and cantilever beam with moving force or moving mass is established. Based on the traditional finite element mass matrix and stiffness matrix, space-time finite element mass matrix and stiffness matrix in each time step is derived by using the iterative scheme to update the displacement and velocity. The dynamic response is calculated with the examples of moving force or moving mass with a certain speed subjected to simply supported beam and cantilever beam. The results are compared with exact solution, Newmark method and Wilson-θmethod, which further demonstrates the effectiveness of space-time finite element method.
     Time-varying dynamics model of the canon barrel with large displacement is established, the corresponding space-time finite element numerical algorithm is deduced. The cradle and barrel are simplified as cantilever beam, moving rigid body, moving spring mass, moving spring rigid body and moving beam. The time domain and space domain is discreted by space-time finite element method, time-varying dynamics equation group is derivated, the dynamic response of the canon barrel with large displacement is calculated through numerical calculation.
     The vibration characteristics of the canon barrel with large displacement is tested and researched. The correctness of theoretical modeling is verified by the results comparing of theoretical calculation and experiment.
     The preliminary research findings of numerical calculation using space-time finite element for the cannon barrel with large displacement achieved in this paper can be of certain reference to in-depth theoretical study on dynamic design of the large displacement time-varying.
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