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Gases and Fluids
Mathematical simulation of hydrocarbon fuel conversion in heat-protection elements of hypersonic aircrafts
A. L. Kuranov, A. V. Korabel'nikov, A. M. Mikhailov Hypersonic System Research Institute, St. Petersburg, Russia
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.
Received: 14.04.2016
Citation:
A. L. Kuranov, A. V. Korabel'nikov, A. M. Mikhailov, “Mathematical simulation of hydrocarbon fuel conversion in heat-protection elements of hypersonic aircrafts”, Zhurnal Tekhnicheskoi Fiziki, 87:1 (2017), 27–33; Tech. Phys., 62:1 (2017), 24–31
Linking options:
https://www.mathnet.ru/eng/jtf6335 https://www.mathnet.ru/eng/jtf/v87/i1/p27
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Statistics & downloads: |
Abstract page: | 30 | Full-text PDF : | 12 |
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