ON THE STABLE METHOD FOR COMPUTING CONICAL FLOW
关于锥型流计算稳定法的讨论

In this paper we presented the computing technique which used the stable me-thod to calculate hypersonic conical flow and applied it to computation of hypersonicflow past a conical body or a triangular wing. Futhermore, the asymptotic conver-gence of solution was proved for the case of a model equation.