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The using of computational modeling for design of gas turbine engines with decreased blowout nitrogen oxides
- Authors: Gulina S.A.1, Orlov M.Y.2, Uglanov D.A.2
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Affiliations:
- Ural State Technical University
- Samara State Aerospace University
- Issue: Vol 7, No 3 (2008): Special Issue
- Pages: 32-35
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/606
- DOI: https://doi.org/10.18287/2541-7533-2008-0-3(16)-32-35
- ID: 606
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Abstract
In this paper it is shown the ways of automatization using in design process of new gas turbine engines with decreased blowout nitrogen oxides.
About the authors
S. A. Gulina
Ural State Technical University
Author for correspondence.
Email: adler65@mail.ru
Russian Federation
M. Y. Orlov
Samara State Aerospace University
Email: adler65@mail.ru
Russian Federation
D. A. Uglanov
Samara State Aerospace University
Email: adler65@mail.ru
Russian Federation
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