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


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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.

作者简介

A. Kuranov

Hypersonic System Research Institute

编辑信件的主要联系方式.
Email: mail@hypersonics.ru
俄罗斯联邦, Moskovskii pr. 212, St. Petersburg, 196066

A. Korabel’nikov

Hypersonic System Research Institute

Email: mail@hypersonics.ru
俄罗斯联邦, Moskovskii pr. 212, St. Petersburg, 196066

A. Mikhailov

Hypersonic System Research Institute

Email: mail@hypersonics.ru
俄罗斯联邦, Moskovskii pr. 212, St. Petersburg, 196066

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