1、 Nodal locations and rotation angles are determined by interpolation.
节点位置和旋转角度由插值确定.
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2、 In addition, the nonlinear iteration semi - analytical nodal method was extended to solve the time - dependent kinetic equations.
另一方面, 本文将非线性迭代半解析节块法扩展应用到时 - 空中子动力学方程组的数值解法中.
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