电邮这篇文章 Thermal state of the shell for supersonic part of the ramjet nozzle
- 作者: Zarubin G.P.1, Zimin V.N.1, Kuvyrkin G.N.1
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隶属关系:
- Moscow State Technical University
- 期: 卷 60, 编号 2 (2017)
- 页面: 236-242
- 栏目: 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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详细
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.
作者简介
G. Zarubin
Moscow State Technical University
编辑信件的主要联系方式.
Email: zarubin@bmstu.ru
俄罗斯联邦, ul. 2-ya Baumanskaya 5, Moscow, 105005
V. Zimin
Moscow State Technical University
Email: zarubin@bmstu.ru
俄罗斯联邦, ul. 2-ya Baumanskaya 5, Moscow, 105005
G. Kuvyrkin
Moscow State Technical University
Email: zarubin@bmstu.ru
俄罗斯联邦, ul. 2-ya Baumanskaya 5, Moscow, 105005
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