Email this article Mathematical simulation of hydrocarbon fuel conversion in heat-protection elements of hypersonic aircrafts
- Authors: Kuranov A.L.1, Korabel’nikov A.V.1, Mikhailov A.M.1
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Affiliations:
- Hypersonic System Research Institute
- Issue: Vol 62, No 1 (2017)
- Pages: 24-31
- Section: 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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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.
About the authors
A. L. Kuranov
Hypersonic System Research Institute
Author for correspondence.
Email: mail@hypersonics.ru
Russian Federation, Moskovskii pr. 212, St. Petersburg, 196066
A. V. Korabel’nikov
Hypersonic System Research Institute
Email: mail@hypersonics.ru
Russian Federation, Moskovskii pr. 212, St. Petersburg, 196066
A. M. Mikhailov
Hypersonic System Research Institute
Email: mail@hypersonics.ru
Russian Federation, Moskovskii pr. 212, St. Petersburg, 196066
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