The supersonic flows are implemented in an axisymmetric channel in many technical devices. These flows are in an expanding part of the nozzle or in the working part of supersonic wind tunnel. The method of supersonic flow calculation in an axisymmetric channel is developed. The method is based on the construction of multi-block axisymmetric grid and linearization of boundary conditions on the aerodynamic surfaces. Testing the method has showed good agreement with known experimental data. The method allows predicting the aerodynamic properties of the aerodynamic form, depending on its location in the channel, as well as the effect of the aerodynamic form on the channel walls in the channel.
 Kashirkin A.A., Maksimov F.A. Sverkhzvukovoe techenie gaza v osesimmetrichnom kanale s prepyatstviyami [Supersonic Gas Flow in AxisymmetricChannel with Obstacles]. Sovremennye problemy aerogidrodinamiki [Modern problems of aerohydrodynamics]. XII school-seminar. Abstracts, Moscow, Moscow State University Publ., 2004, p. 56.
 Maksimov F.A. Izvestiya Tulskogo gosudarstvennogo universiteta Seriya Problemy spetsialnogo mashinostroeniya – Proceedings of the Tula State University. Series: Problems of Special machinery Engineering, 2001, vol. 4, no. 1, pp. 257–261.
 Dunaev V.A., Maximov F.A. Modelirovanie sverkhzvukovykh techeniy nevyazkogo gaza [Simulation of Supersonic Non-viscid Gas Flows]. Tula, Tula State University Publ., 2006, 180 p.
 Kosykh A.P., Minaylos A.N. Aerodinamicheskie kharakteristiki krylyev prosteyshikh form na sverkhzvukovykh skorostyakh [The Aerodynamic Characteristics of the Simplest Form Wings at Supersonic Speeds]. Proceedings of the Central Aerohydrodynamics Institute, 1977, no. 1891.
Maksimov F. Supersonic flow in axisymmetric channel. Маthematical Modeling and Coтputational Methods, 2015, №1 (5), pp. 109-120
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