建立了一个全耦合的机身对旋翼气动干扰的迭代计算方法。
A full coupled and iterative analytical method has been developed to investigate the aerodynamic interaction of a helicopter fuselage on its rotor.
利用半解析节块法的非线性迭代计算方法求解多维多群中子扩散方程。
The application of nonlinear iteration semi-analytic nodal method in CANDU reactor fuel management;
用这组方程和迭代计算方法，能够求解各种类型的振幅和相位的恢复问题。
Using these equations and the iteration computing method, a variety of reconstruction problems can be solved.
应用推荐