Literature cited
R. E. Oliver, “On experimental investigation of flow about simple blunt bodies at nominal Mach number of 5.8,” J. Aero. Sci.,23, No. 2 (1956).
G. L. Grodzovskii, “Some peculiarities of the flow over bodies at large supersonic velocities,” Izv. Akad. Nauk SSSR, OTN, No. 6, (1957).
W. D. Hayes and R. F. Probstein, Hypersonic Flow Theory, Academic Press (1959).
Theory of Optimum Aerodynamic Shapes, Academic Press (1965).
F. L. Chernous'ko, “The method of local variations for the numerical solution of variational problems,” Zh. Vychisl. Matem. i Matem. Fiz.,5, No. 4 (1965).
V. D. Perminov, “Wings of given volume with maximum aerodynamic performance in a hypersonic flow,” Izv. AN SSSR, Mekhan. Zhidk. i Gaza, No. 5 (1969).
V. D. Perminov, “Wings of optimum characteristics in a hypersonic flow,” Izv. AN SSSR, Mekhan. Zhidk. i Gaza, No. 6 (1969).
Present State of High-Velocity Aerodynamics [Russian translation], IL, Moscow (1955).
A. L. Ankudinov, “Boundary-layer calculations on blunted cones in a supersonic flow,” Zh. Vychisl. Matem. i Matem. Fiz.,5, No. 5 (1965).
N. M. Belyanin, “Determination of the shape of a body with minimum heat flow for laminar boundary-layer flow,” Izv. AN SSSR, Mekhan. Zhidk. i Gaza, No. 6 (1967).
G. G. Chernyi, “Hypersonic flow over wings at high angles of attack,” Dokl. Akad. Nauk SSSR,155, No. 2 (1964).
G. L. Grodzovskii, “On bodies of revolution with a minimum frontal-resistance coefficient and small heat transfer at high supersonic speeds,” Izv. AN SSSR, Mekhan. Zhidk. i Gaza, No. 5 (1968).
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 1, pp. 90–96, January–February, 1971.
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Perminov, V.D. Axially symmetric body of minimum resistance in a viscous hypersonic flow. Fluid Dyn 6, 80–85 (1971). https://doi.org/10.1007/BF01045910
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DOI: https://doi.org/10.1007/BF01045910