Engineering Journal: Science and InnovationELECTRONIC SCIENCE AND ENGINEERING PUBLICATION
Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
  • Русский
  • Английский
Article

Features of high-speed aircraft numerical simulation

Published: 17.01.2020

Authors: Alekseeva M.M., Brykov N.A., Vikhrova I.A.

Published in issue: #1(97)/2020

DOI: 10.18698/2308-6033-2020-1-1946

Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts

Currently, the creation of new high-speed aircraft is of great interest. The development of such aircraft is associated with the need for experiments and flight tests. The organization of real physical experiments in the field of high speeds is fraught with significant difficulties that can be solved using the numerical simulation method, which makes it possible to significantly simplify the process of creating new products. When developing a high-speed aircraft, it is necessary to take into account the specific aerodynamic and thermophysical features of the processes occurring on the surface of the aircraft and in the shock layer. In this paper, the features of the processes at high speeds are considered on the example of solving the external and internal problems of the gas dynamics of an aircraft. Based on the specifics of these processes, we built a mathematical model that allows us to study the aerodynamics of a high-speed flow around a body in dense layers of the atmosphere and the processes that occur in the combustion chamber.


References
[1] Reubush D.E., Nguyen L.T., Rausch V.L. Review of X-43A return to flight activities and current status. In: 12th AIAA International Space Planes and Hypersonic Systems and Technologies, International Space Planes and Hypersonic Systems and Technologies Conf. (Norfolk, Virginia), 2003. AIAA 2003-7085.
[2] Ferlemann S.M., McClinton C.R., Rock K.E., Voland R.T. Hyper X Mach 7 Scramjet Design, Ground Test and Flight Results. In: AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies, AIAA 2005-3322. https://doi.org/10.2514/6.2005-3322
[3] Volkov K.N., Emelyanov V.N., Karpenko A.G. Vychislitelnye metody i programmirovanie — Numerical Methods and Programming, 2017, vol. 18, no. 4, pp. 387–405.
[4] Scanlon T.J., White C., Borg M.K., Palharini R.C., Farbar E., Boyd I.D., Reese J.M., Brown R.E. Open-Source Direct Simulation Monte Carlo chemistry modeling for hypersonic flows. AIAA Journal, 2014. https://doi.org/10.2514/1.J053370
[5] Dubois J. Radiation calculation in non-equilibrium shock layer. In: Proceedings of the International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, 2004, Part II (ESA SP-583), pp. 41–47.
[6] Surzhikov S.T. Vestnik MGTU im. N.E. Baumana. Ser. Mashinostroenie — Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, 2005, no. 3, pp. 7–33.
[7] Sinha К., Vadivelan С. Effect of angle of attack on re-entry capsule after body flow field. In: Proceedings of 46th American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting and Exhibit. Reno, Nevada, USA, 7–10 January, 2008, AIAA Paper 2008-1282.
[8] Zheleznyakova A.L., Surzhikov S.T. Vestnik MGTU im. N.E. Baumana. Ser. Mashinostroenie — Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, 2009, no. 2, pp. 3–25.
[9] Borisov V.E. Preprinty IPM im. M.V. Keldysha no. 137 — Keldysh Institute Preprints no. 137. Moscow, 2016, pp. 3–12.
[10] Zheleznyakova A.L., Surzhikov S.T. TVT — High Temperature, 2013, vol. 51, no. 5, pp. 1–15.
[11] Van Dyke M. An Album of Fluid Motion. The Parabolic Press, 175 p. [In Russ.: Van Dyke M. Albom techenii zhidkosti i gaza. Moscow, Mir Publ., 1986].