一维气体动力学问题的半解析隐式直接时间积分法

Igor Orynyak, Iryna Kostyushko, Roman Mazuryk
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引用次数: 0

摘要

一维气体动力学问题的锐波处理仍然是现代数值方法的一个挑战。它们通常需要太多的空间和时间步长,导致解的伪振荡,表现出很强的数值耗散或结果发散。本文是作者利用空间坐标解析解的思想的进一步推广,其中时间步长是空间解中的一个参数。它的特点在于对压力和密度之间的相关性进行线性化的附加程序的发展。其前提是每个空间单元的实际压力接近于前一时刻的基本压力。该方法的有效性在非常流行的Sod任务中得到了测试,该任务是用隔膜将管中的两种不同的理想气体分开,而隔膜突然断裂。拉格朗日坐标公式中考虑的问题。结果表明,该方法具有较好的效率,所需的时间和空间步长都较短,不会产生伪振荡,网格划分结果一致且可预测。方法的精度主要由时间步长控制,时间步长应大于明确规定的理论下限。该方法的另一个优点是可以将过程计算到所需的任何时刻,并且空间网格划分可以随时间和空间变化,在计算过程中可以方便地进行调整。
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Semi-analytical implicit direct time integration method for 1-D gas dynamic problem
Sharp wave treatment for 1-D gas dynamic problem is still a chellenge for modern numerical methods. They often require too many space and time steps, produce spurious oscillation of solution, exhibit a strong numerical dissipation or divergence of results. This paper is further extension of authors’ idea of employment the analytical solution for space coordinate, where time step is a parameter which used in the space solution. Its peculiarity consists in development of additional procedure of linearization of dependence between the pressure and density. It is performed in premise that actual pressure for each space element is close to the basic pressure, attained at previous moment of time. The efficiency of method is tested on the very popular task of Sod, where two different ideal gases in a tube are separated by diaphragm, which is suddenly broken. The problem considered in Lagrangian coordinates formulation. The results obtained show the very good efficiency of method, which requires the essentially lesser time and space steps, leads to no spurious oscillation and give consistent and predictable results with respect to meshing. The accuracy of method is mostly controlled by time step, which should be larger than clearly stated theoretical lower limit. Other advantage of method is that it can calculate the process to any desired moment of time, and space meshing can be variable in time and space and can be easily adapted during the process of calculation.
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