Enviar artigo por via de e-mail Thermal state of the shell for supersonic part of the ramjet nozzle
- Autores: Zarubin G.P.1, Zimin V.N.1, Kuvyrkin G.N.1
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Afiliações:
- Moscow State Technical University
- Edição: Volume 60, Nº 2 (2017)
- Páginas: 236-242
- Seção: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230099
- DOI: https://doi.org/10.3103/S106879981702012X
- ID: 230099
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Resumo
A mathematical model describing the temperature distribution in a non-cooled nozzle shell was constructed. Analysis of this model showed that the extreme temperatures are permissible for some modern and promising heat-resistant composite materials.
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Sobre autores
G. Zarubin
Moscow State Technical University
Autor responsável pela correspondência
Email: zarubin@bmstu.ru
Rússia, ul. 2-ya Baumanskaya 5, Moscow, 105005
V. Zimin
Moscow State Technical University
Email: zarubin@bmstu.ru
Rússia, ul. 2-ya Baumanskaya 5, Moscow, 105005
G. Kuvyrkin
Moscow State Technical University
Email: zarubin@bmstu.ru
Rússia, ul. 2-ya Baumanskaya 5, Moscow, 105005
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