Mathematical simulation of hydrocarbon fuel conversion in heat-protection elements of hypersonic aircrafts

We consider a mathematical model of hydrocarbon fuel conversion in a thermochemical reactor as an element of heat protection of a hypersonic aircraft. The application of this model has made it possible to enrich information obtained in experimental studies.

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Published in:	Technical physics Vol. 62; no. 1; pp. 24 - 31
Main Authors:	Kuranov, A. L., Korabel’nikov, A. V., Mikhailov, A. M.
Format:	Journal Article
Language:	English
Published:	Moscow Pleiades Publishing 2017 Springer Springer Nature B.V
Subjects:	Analysis Classical and Continuum Physics Combustion Computer simulation Conversion Gases and Liquids Hydrocarbons Hypersonic aircraft Mathematical analysis Mathematical models Nuclear fuels Numerical analysis Physics Physics and Astronomy
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Abstract	We consider a mathematical model of hydrocarbon fuel conversion in a thermochemical reactor as an element of heat protection of a hypersonic aircraft. The application of this model has made it possible to enrich information obtained in experimental studies.
AbstractList	We consider a mathematical model of hydrocarbon fuel conversion in a thermochemical reactor as an element of heat protection of a hypersonic aircraft. The application of this model has made it possible to enrich information obtained in experimental studies. DOI: 10.1134/S1063784217010157 We consider a mathematical model of hydrocarbon fuel conversion in a thermochemical reactor as an element of heat protection of a hypersonic aircraft. The application of this model has made it possible to enrich information obtained in experimental studies.
Audience	Academic
Author	Mikhailov, A. M. Kuranov, A. L. Korabel’nikov, A. V.
Author_xml	– sequence: 1 givenname: A. L. surname: Kuranov fullname: Kuranov, A. L. email: mail@hypersonics.ru organization: Hypersonic System Research Institute – sequence: 2 givenname: A. V. surname: Korabel’nikov fullname: Korabel’nikov, A. V. organization: Hypersonic System Research Institute – sequence: 3 givenname: A. M. surname: Mikhailov fullname: Mikhailov, A. M. organization: Hypersonic System Research Institute
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References	H. Lander and A. Nixon, AIAA Pap. 997, 1 (1968). KuranovA. L.Korabel’nikovA. V.MikhailovA. M.Principal Design and Modeling of Thermal Protection for Hypersonic Vehicles2014St. PetersburgIzd. Politekh. Univ. MikhailovA. M.Nauchno-Tekh. Vedomosti S.-Peterb. Gos. Univ.2013317895 KuranovA. L.Korabel’nikovA. V.MikhailovA. M.Proceedings of the 5th European Conference on Aeronautics and Space Sciences EUCASS2013 KuranovA. L.Korabel’nikovA. V.MikhailovA. M.Tech. Phys. Lett.201440912014TePhL..40...91K10.1134/S1063785014010258 Bal’minaR. V.GubanovA. A.Ivan’kinM. A.LapinskiiD. A.TsAGI Tekh. Inform. Novosti Zarub. Nauki Tekh., Ser.: Aviats. Raketnaya Tekh.20121–21821 VargaftikN. B.Thermal Properties of Gases and Fluids: A Handbook1972MoscowNauka AleksandrovA. A.Grigor’evB. A.Tables of Heat Quantities of Water and Vapor: A Handbook1999MoscowIzd. Mosk. Energ. Inst. New Handbook of a Chemist and Technologist: Electrode Processes, Chemical Kinetics and Diffusion, Colloidal Chemistry, Ed. by S. A. Simanova (Professional, St. Petersburg, 2004). MaslenkovS. B.Heat-Resistant Steels and Alloys: A Handbook1983 S. B. Maslenkov (1378_CR8) 1983 1378_CR2 R. V. Bal’mina (1378_CR1) 2012; 1–2 A. A. Aleksandrov (1378_CR9) 1999 A. L. Kuranov (1378_CR5) 2014; 40 A. L. Kuranov (1378_CR3) 2014 A. L. Kuranov (1378_CR6) 2013 N. B. Vargaftik (1378_CR7) 1972 A. M. Mikhailov (1378_CR4) 2013; 3 1378_CR10
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SubjectTerms	Analysis Classical and Continuum Physics Combustion Computer simulation Conversion Gases and Liquids Hydrocarbons Hypersonic aircraft Mathematical analysis Mathematical models Nuclear fuels Numerical analysis Physics Physics and Astronomy
Title	Mathematical simulation of hydrocarbon fuel conversion in heat-protection elements of hypersonic aircrafts
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