1.
The back EMF constant and torque constant are analyzed. The calculating formulas are gived.
分析了电机的反电势常数和力矩常数,并给出了计算公式;
2.
The general solution and derivative matrix formulations of axial and transverse displacement function has been established by regarding fhe axial and transverse reaction coeflicients od stratification foundation as constants respectively.
分别采用各层地基竖向、向反力系数为常数，建立轴向、向位移函数通解及导数的矩阵式。
3.
Method for matrix solution of constant coefficient recursive sequences general term equation;
常系数递归数列通项公式的矩阵求法
4.
A Numerical Algorithm of Singular Integrals over Rectangular Domains
矩形域上非正常积分的一种数值算法
5.
Next, define the constant elements hij of the nn hessian matrix H
其次，定义n×n海赛矩阵H的常数元数为hij。
6.
The Design and Research of Digital-indicate Planetary Gear Multiplier Wrench;
数显式行星力矩放大扳手的设计研究
7.
Study on Parameters Optimization and Shaping of the Hydrodynamic Torque Converter Blade;
液力变矩器叶栅参数优化及造型研究
8.
Numerical Simulation Analysis of Torque Converter's Internal Flow Field
液力变矩器内部流场的数值模拟分析
9.
Optimization of Torque Converter's Blade Angle Parameter and Arithmetic
液力变矩器叶栅角度参数优化及算法
10.
Calculation of Basic Solution Matrix of Linear Homogeneous System with Constant Coefficients
常系数齐次线性微分方程组基解矩阵的求解
11.
On Matrix Solution to Initial Value Problem of an N-th Order Linear Constant Coefficient Differential Equation;
n阶线性常系数微分方程初值问题的矩阵解法
12.
Toeplitz matrix for inhomogeneous linear difference equation with constant coefficients
Toeplitz矩阵在常系数线性差分方程中的应用
13.
The solution of ordinary differential equation with constant coefficients using up-triangular Toeplitz matrix
利用上三角Toeplitz矩阵求常系数微分方程的特解
14.
Research on Analysing and Compensation of the Steady Disturbing Torque of the Three Axis Air Bearing Table
三轴气浮平台常值干扰力矩的分析与补偿
15.
3D Numerical Analysis of Bearing Capacity Shape Factors for Rectangular Footings
矩形基础承载力形状系数三维数值模拟
16.
Study on Axial Force in Hydrodynamic Torque Converter Based on Numerical Solution of Three-Dimensional Flow Field;
基于三维流场数值解的液力变矩器轴向力研究
17.
The aerodynamic terms in the force and moment equations have all been replaced by the state variables of which they are functions. and control forces and moments.
力和力矩方程中的空气动力项已经全部用为其函数的状态变量及操纵力和力矩所代替。
18.
" Flight mechanics--Concepts,quantities and symbols--Forces, moments, their coefficients and derivatives"
GB/T14410.2-1993飞行力学概念、量和符号力、力矩及其系数和导数