Applied Mathematics and Mechanics (English Edition) ›› 1983, Vol. 4 ›› Issue (1): 55-68.
张涵信, 陆林生, 余泽楚, 马占奎
Zhang Han-xin, Lu Lin-sheng, Yu Ze-chu, Ma Zhan-kui
摘要: The supersonic and hypersonic,laminar and turbulent viscous separated flows over two and three-dimensional compression corners are solved by the antidissipative explicit-implicit difference scheme presented in this paper. The results obtained show that a high accuracy has been achieved by this method and the time needed for computation is greatly reduced.