By use of numerical approximation method, the paper USES the polynomial to approach segmentally the transient electric field from dipole dipole array.
本文采用数值逼近的方法，逐段用多项式表示偶极—偶极排列的瞬变电场。
Numerical computations show that paraxial approximation gives almost the same accuracy in the paraxial region as complex ray method but spends much less computer time.
所得数字结果表明，在波束的近轴区域内为获得同样的计算精度，近轴近似法所需要的计算机时间远小于复射线追综法的时间。
Some numerical examples are given to show that the numerical method presented is an approximation method with high efficiency and convergence.
数值计算表明本文数值方法是一种高效和收敛的近似方法。
Numerical computations show that paraxial approximation gives almost the same accuracy in the paraxial region as complex ray method but spends much...
所得数字结果表明，在波束的近轴区域内为获得同样的计算精度，近轴近似法所需要的计算机时间远小于复射线追综法的时间。
A hybrid technique for calculating the scattering of two-dimensional large bodies with slots is developed by combining high-frequency approximation method with low-frequency numerical method.
本文利用高频近似方法与低频数值方法相结合的混合方法计算二维开槽电大目标的散射。
The values of the settlement are approximation with calculated value of summating for each layer and calculated values on prototype of numerical analysis. Therefore, this method is very feasible.
模型试验实测沉降量与用分层总和法、数值分析法计算结果接近。
The predictive intelligent control scheme is proposed, which is based on approximation theory and numerical method of Chcbyshev orthogonal polynomial.
本文基于切比雪夫正交多项式数值逼近方法，提出预测智能控制算法。
The approximation of the numerical results to the spot test results demonstrates the feasibility and effectiveness of the presented method.
计算结果与实测结果的接近验证了本文方法的可行有效性。
A meshless method using the moving least squares approximation is improved and applied to the numerical computation of electromagnetic fields.
本文将无网格算法推广应用于电磁场的数值计算。
A numerical method is presented for predicting the aerodynamic characteristics of elastic aircraft under quasi-static approximation.
本文介绍一种准静弹性飞机气动特性的数值计算方法。
A numerical method is presented for predicting the aerodynamic characteristics of elastic aircraft under quasi-static approximation.
本文介绍一种准静弹性飞机气动特性的数值计算方法。
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