The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.

摘要一实验电弧加热式发动机二维称亚跨超音速流动进了数值模拟，所采用的方法是矢通量分裂算法。

Axisymmetric elasticity problem of cubic quasicrystal is reduced to a solution of a partial differential equation with higher-order by introducing displacement function.

本通过引入位移函数使得立方准晶的称弹性问题化求解一高阶偏微分方程。

The analysis of the finite element method using th e axisymmetric model was employed to assess the mechanics behavior of the rubber toughening in mesostructure.

在细观结构上采用典型称单元的有限元分析来预测增韧环氧树脂的力。

The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.

摘要对一实验电弧加热式发动机二维轴对称亚跨超音速流动进值模拟，所采用的方法是矢通量分裂算法。

Axisymmetric elasticity problem of cubic quasicrystal is reduced to a solution of a partial differential equation with higher-order by introducing displacement function.

本通过引入位移函使得立方准晶的轴对称题化为求解一高阶偏微分方程。

The analysis of the finite element method using th e axisymmetric model was employed to assess the mechanics behavior of the rubber toughening in mesostructure.

在细观结构上采用典型轴对称单元的有限元分析来预测增韧环氧树脂的力学为。

The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.

摘要对一实验电弧加热式发动机二维轴对称亚跨超音速流动进行了数值模拟，所采的方法是矢通量分裂算法。

Axisymmetric elasticity problem of cubic quasicrystal is reduced to a solution of a partial differential equation with higher-order by introducing displacement function.

本通过引入位移函数使得立方准晶的轴对称弹性问题化为求解一高阶偏微分方程。

The analysis of the finite element method using th e axisymmetric model was employed to assess the mechanics behavior of the rubber toughening in mesostructure.

在细观结构上采典型轴对称单元的有限元分析来预测增树脂的力学行为。

The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.

摘要对一实验电弧加热式发动机二维轴对称亚跨超音速流动进行了数值模拟，所采用的方法是矢量分裂算法。

Axisymmetric elasticity problem of cubic quasicrystal is reduced to a solution of a partial differential equation with higher-order by introducing displacement function.

引入位移函数使得立方准晶的轴对称弹性问题化为求解一高阶偏微分方程。

The analysis of the finite element method using th e axisymmetric model was employed to assess the mechanics behavior of the rubber toughening in mesostructure.

在细观结构上采用典型轴对称单元的有限元分析来预测增韧环氧树脂的力学行为。

The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.

摘要一实验电弧加热式发动机二维亚跨超音速流动进行了数值模拟，所采用的方法是矢通量分裂算法。

Axisymmetric elasticity problem of cubic quasicrystal is reduced to a solution of a partial differential equation with higher-order by introducing displacement function.

本通过引入位移函数使得立方准晶的弹性问题化为求解一高阶偏微分方程。

The analysis of the finite element method using th e axisymmetric model was employed to assess the mechanics behavior of the rubber toughening in mesostructure.

在细观结构上采用典型单元的有限元分析增韧环氧树脂的力学行为。

The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.

摘要一实验电弧加热式发动机二维称亚跨超音速流动进行了数值，所采用方法是矢通量分裂算法。

Axisymmetric elasticity problem of cubic quasicrystal is reduced to a solution of a partial differential equation with higher-order by introducing displacement function.

本通过引入位移函数使得立方准晶称弹性问题化为求解一高阶偏微分方程。

The analysis of the finite element method using th e axisymmetric model was employed to assess the mechanics behavior of the rubber toughening in mesostructure.

在细观结构上采用典型称单元有限元分析来预测增韧环氧树脂力学行为。

The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.

摘要对一实验电弧加热式发动机二维轴对称亚跨超音速流动进值模拟，所采用的方法是矢通量分裂算法。

Axisymmetric elasticity problem of cubic quasicrystal is reduced to a solution of a partial differential equation with higher-order by introducing displacement function.

本通过引入位移函使得立方准晶的轴对称题化为求解一高阶偏微分方程。

The analysis of the finite element method using th e axisymmetric model was employed to assess the mechanics behavior of the rubber toughening in mesostructure.

在细观结构上采用典型轴对称单元的有限元分析来预测增韧环氧树脂的力学为。

The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.

摘要对一实验电弧加热式发动机二维对称亚跨超音速流动进行了数值模拟，所采的方法是矢通量分裂算法。

Axisymmetric elasticity problem of cubic quasicrystal is reduced to a solution of a partial differential equation with higher-order by introducing displacement function.

本通过引入位移函数使得立方准晶的对称弹性问题化为求解一高阶偏微分方程。

The analysis of the finite element method using th e axisymmetric model was employed to assess the mechanics behavior of the rubber toughening in mesostructure.

在细观结构上采典型对称单元的有限元分析来预环氧树脂的力学行为。

The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.

摘要对实验电弧加热式发动机二维轴对称亚跨流动进行了数值模拟，所采用的方法是矢通量分裂算法。

Axisymmetric elasticity problem of cubic quasicrystal is reduced to a solution of a partial differential equation with higher-order by introducing displacement function.

本通过引入位移函数使得立方准晶的轴对称弹性问题化为高阶偏微分方程。

The analysis of the finite element method using th e axisymmetric model was employed to assess the mechanics behavior of the rubber toughening in mesostructure.

在细观结构上采用典型轴对称单元的有限元分析来预测增韧环氧树脂的力学行为。