Enviar artigo por via de e-mail Mathematical simulation of hydrocarbon fuel conversion in heat-protection elements of hypersonic aircrafts
- Autores: Kuranov A.L.1, Korabel’nikov A.V.1, Mikhailov A.M.1
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Afiliações:
- Hypersonic System Research Institute
- Edição: Volume 62, Nº 1 (2017)
- Páginas: 24-31
- Seção: Gases and Liquids
- URL: https://bakhtiniada.ru/1063-7842/article/view/198735
- DOI: https://doi.org/10.1134/S1063784217010157
- ID: 198735
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Resumo
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.
Sobre autores
A. Kuranov
Hypersonic System Research Institute
Autor responsável pela correspondência
Email: mail@hypersonics.ru
Rússia, Moskovskii pr. 212, St. Petersburg, 196066
A. Korabel’nikov
Hypersonic System Research Institute
Email: mail@hypersonics.ru
Rússia, Moskovskii pr. 212, St. Petersburg, 196066
A. Mikhailov
Hypersonic System Research Institute
Email: mail@hypersonics.ru
Rússia, Moskovskii pr. 212, St. Petersburg, 196066
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