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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Bibliographic Details
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
Online Access:	Get full text
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Description
Summary:	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.
ISSN:	1063-7842 1090-6525
DOI:	10.1134/S1063784217010157