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Numerical Simulation of the Exit Temperature Pattern of an Aircraft Engine Using a Temperature-Dependent Turbulent Schmidt Number Cover

Numerical Simulation of the Exit Temperature Pattern of an Aircraft Engine Using a Temperature-Dependent Turbulent Schmidt Number

Open Access
|Oct 2021

Authors

Igor F. Kravchenko

SE “Ivchenko-Progress”, Zaporozhye, Ukraine

Dmytro V. Kozel

kozeldv@ivchenko-progress.com

SE “Ivchenko-Progress”, Zaporozhye, Ukraine

Serhii A. Yevsieiev

SE “Ivchenko-Progress”, Zaporozhye, Ukraine
Language: English
Page range: 34 - 46
Published on: Oct 8, 2021
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2021 Igor F. Kravchenko, Dmytro V. Kozel, Serhii A. Yevsieiev, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.