1. A. N. Kraiko, D. E. Pudovikov, K. S. P’yankov, and N. I. Tillyaeva, “Axisymmetric noses with a given aspect ratio optimal and near-optimal for wing drag,” Prikl. Mat. Mekh., 67, 795 (2003).
2. A. J. Eggers Jr., M. M. Resnikoff, and D. H. Dennis, “Bodies of revolution having minimum drag at high supersonic air speeds,” NACA Report, No. 1306 (1957).
3. G. L. Grozdovskii (ed.), Aeromechanics of the Supersonic Flow past Power-Law Bodies of Revolution [in Russian], Mashinostroenie, Moscow (1975).
4. S. A. Takovitskii, “Analytical solution in the problem of constructing an airfoil with minimum drag,” Fluid Dynamics, 38, No. 6, 933 (2003).
5. S. A. Takovitskii, “Constructing axisymmetric noses with minimum wave drag,” Prikl. Mat. Mekh., 71, No. 3 (2003).