采用SIMPL E算法的可压缩形式求解固体火箭发动机燃烧室喷管内的全速度统一流场;
United flow field at all flow speeds in the chamber and nozzle of SRM is solved by using the compressible form of the SIMPLE algorithm.
对非线性不等式约束最优化问题进行了讨论,借助广义投影建立求解问题的一个含系列自由参数的统一算法模型。
Optimization problem with nonlinear inequality constraints is discussed. With the help of the generalized projection, a unified algorithm model with a series of free parameters is presented.
提出了一种求解微分代数混合方程组的统一算法,证明了统一算法所求出的懈与原方程组的解具有等价性。
This article present an unification arithmetic for a kind of mixture equations made up of some differential and algebra equations.
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