Email this article Thermal state of the shell for supersonic part of the ramjet nozzle
- Authors: Zarubin G.P.1, Zimin V.N.1, Kuvyrkin G.N.1
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Affiliations:
- Moscow State Technical University
- Issue: Vol 60, No 2 (2017)
- Pages: 236-242
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230099
- DOI: https://doi.org/10.3103/S106879981702012X
- ID: 230099
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Abstract
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.
About the authors
G. P. Zarubin
Moscow State Technical University
Author for correspondence.
Email: zarubin@bmstu.ru
Russian Federation, ul. 2-ya Baumanskaya 5, Moscow, 105005
V. N. Zimin
Moscow State Technical University
Email: zarubin@bmstu.ru
Russian Federation, ul. 2-ya Baumanskaya 5, Moscow, 105005
G. N. Kuvyrkin
Moscow State Technical University
Email: zarubin@bmstu.ru
Russian Federation, ul. 2-ya Baumanskaya 5, Moscow, 105005
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