JACOBIAN MATRIX SPLITTING METHODS AND NUMERICAL COMPUTATION OF AERODYNAMICS EQUATIONS
Jacobian系数矩阵分裂法与气动方程的数值计算

The flux vector splitting technique is widely used in solving aerodynamics equations. Inthe present paper different Jacobian matrix splitting methods are considered. By Taylor ex-pansion series, different differnce schemes are obtained which are linear and requires nospecial linearization, Then, Simple and efficient implicit difference schemes are obtained withspecially chosen matrix splitting. Practical applications show that the suggested method is ef-ficient.