Email this article Integration of a High-Pressure Gas Turbine of the Gas Turbine Engine with a Gas-Dynamic Laser
- Authors: Perel’shtein B.K.1, Osipov B.M.1, Titov A.V.1
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Affiliations:
- Kazan State Power Engineering University
- Issue: Vol 61, No 4 (2018)
- Pages: 687-691
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230786
- DOI: https://doi.org/10.3103/S1068799818040293
- ID: 230786
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Abstract
The approaches to integration of a high-pressure super-reaction turbine of an aircraft gas turbine engine and a gas-dynamic laser are considered.
About the authors
B. Kh. Perel’shtein
Kazan State Power Engineering University
Author for correspondence.
Email: perel.boris@gmail.com
Russian Federation, ul. Krasnosel’skaya 51, Kazan, 420066
B. M. Osipov
Kazan State Power Engineering University
Email: perel.boris@gmail.com
Russian Federation, ul. Krasnosel’skaya 51, Kazan, 420066
A. V. Titov
Kazan State Power Engineering University
Email: perel.boris@gmail.com
Russian Federation, ul. Krasnosel’skaya 51, Kazan, 420066
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