Some computational data and figures are presented.
并给出了相应的计算数据和图示。
Upon the computational data flow model, the error flow model is set up.
在计算数据流模型的基础上，进一步建立了错误流模型。
Then compute aerodynamic drag of high temperature particle at different temperature difference and fit the formula according to the computational data points.
计算了颗粒与气体不同温差情况下高温颗粒的气动阻力，并根据计算数据点拟合了计算公式。
The accuracy of theoretical calculation model has been verified through the comparison and analysis between experiment data and theoretical computational data.
通过实测实验数据和理论计算数据的对比分析，验证了计算模型的正确性。
The paper computes the cutoff wavelength and field pattern at different ridge positions in asymmetric single ridge waveguide and L-shape waveguide. Some computational data and figures are presented.
文中编程计算了不对称脊波导、L型波导脊位置变化时截止波长和场结构的变化规律，给出了计算数据和曲线图。
The paper computes the cutoff wavelength and field pattern at different ridge positions in asymmetric single ridge waveguide and L-shape waveguide. Some computational data and figures are presented.
文中编程计算了不对称脊波导、L型波导脊位置变化时截止波长和场结构的变化规律，给出了计算数据和曲线图。
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