1. M.D. Van Dyke, A model of supersonic flow past blunt axisymmetric bodies, with application to Chester’s solution, J. Fluid Mech., 1958, Vol. 3, Iss. 5, P. 515-522.
2. W.E. Moeckel, Approximate method for predicting form and location of detached shock waves ahead of plane or axial symmetric bodies, NACA Techn. Note, 1949, No. TN-1921.
3. J.W. Heberle, G.P. Wood, and P.B. Gooderum, Data on shape and location of detached shock waves on cones and spheres, Report NASA, 1950, No. TM-2000.
4. M.D. Van Dyke, The supersonic blunt-body problem-review and extensions, J. Aeronaut. Sci., 1958, P. 485-496.
5. H.W. Liepmann and A. Roshko, Elements of Gasdynamics., John Wiley & Sons, N.Y., 1957.