1. Three-dimensional compressible laminar boundary-layer flow;Moore;NACA Tech. Note No. 2279,1951
2. Laminar boundary layer on cone in supersonic flow at large angle of attack;Moore;NACA Rept. No. 1132,1953
3. The shock layer concept and three-dimensional hypersonic boundary layers;Cheng;Cornell Aero. Lab. Rept. AF-1285-A-3,1961
4. Supersonic laminar boundary layer near the plane of symmetry of a cone at incidence;Roux;J. Fluid Mech.,1972
5. The solution of sharp-cone boundary-layer equations in the plane of symmetry;Murdock;J. Fluid Mech.,1972