电邮这篇文章 Integration of a High-Pressure Gas Turbine of the Gas Turbine Engine with a Gas-Dynamic Laser
- 作者: Perel’shtein B.K.1, Osipov B.M.1, Titov A.V.1
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隶属关系:
- Kazan State Power Engineering University
- 期: 卷 61, 编号 4 (2018)
- 页面: 687-691
- 栏目: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230786
- DOI: https://doi.org/10.3103/S1068799818040293
- ID: 230786
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详细
The approaches to integration of a high-pressure super-reaction turbine of an aircraft gas turbine engine and a gas-dynamic laser are considered.
作者简介
B. Perel’shtein
Kazan State Power Engineering University
编辑信件的主要联系方式.
Email: perel.boris@gmail.com
俄罗斯联邦, ul. Krasnosel’skaya 51, Kazan, 420066
B. Osipov
Kazan State Power Engineering University
Email: perel.boris@gmail.com
俄罗斯联邦, ul. Krasnosel’skaya 51, Kazan, 420066
A. Titov
Kazan State Power Engineering University
Email: perel.boris@gmail.com
俄罗斯联邦, ul. Krasnosel’skaya 51, Kazan, 420066
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