Study of performance of the aircraft gas turbine engine integrated with a gas dynamic laser-Reference-Cited by-同舟云学术

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Study of performance of the aircraft gas turbine engine integrated with a gas dynamic laser

Published:2017-07 Issue:3 Volume:60 Page:474-477
ISSN:1068-7998
Container-title:Russian Aeronautics
language:en
Short-container-title:Russ. Aeronaut.

Author:

Osipov B. M.,Kopelevich L. A.,Perel’shtein B. Kh.

Publisher

Allerton Press

Subject

Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.3103/S1068799817030230.pdf

Reference11 articles.

1. Translucator for Ecilop, URL: https://nplus1.ru/news/2015/04/28/lasers.

2. Perel’shtein, B. Kh., RU Patent 2516985, Byul.Izobr., 2014, no. 15.

3. Vovk, M.Yu., Marchukov, E.Yi., Petrenko, V.G., and Perel’shtein, B. Kh., RU Patent 2587509, Byul.Izobr., 2016, no. 17.

4. Perel’shtein, B. Kh., Novye energeticheskie sistemy (New Energy Systems), Kazan: Kazan State Technical University Publishing, 2008.

5. Perel’shtein, B., New Energy Systems, URL: https://www.ljubljuknigi.ru/store/ru/book/1/isbn/978-3-659-74713-7.

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1. Design and Implementation of High-Power Gas Dynamic Laser Nozzle Unit Based on Aero-Optics;2022 International Telecommunications Conference (ITC-Egypt);2022-07-26

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