A direct method for calculation of the flow about an axisymmetric blunt body at angle of attack.
暂无分享,去创建一个
[1] P. H. Rose,et al. Feasibility of a High-Performance Aerodynamic Impulse Facility , 1968 .
[2] M. V. Dyke,et al. The Supersonic Blunt-Body Problem - Review and Extension , 1958 .
[3] TRANSONIC ROTATIONAL FLOW OVER A CONVEX CORNER , 1960 .
[4] M. Dunn,et al. Effects of mass injection on compressible, three-dimensional, laminar boundary layers. , 1967 .
[5] B. Adler,et al. Inverse solution of blunt-body flowfields at large angle of attack. , 1967 .
[6] I. Bohachevsky,et al. A direct method for computation of nonequilibrium flows with detached shock waves. , 1965 .
[7] P. Lax. Weak solutions of nonlinear hyperbolic equations and their numerical computation , 1954 .