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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

Transactions on Aerospace Research
Volume 2021 (2021): Issue 3 (September 2021)
By: Igor F. Kravchenko,  Dmytro V. Kozel and  Serhii A. Yevsieiev  
Open Access
|Oct 2021
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DOI: https://doi.org/10.2478/tar-2021-0015 | Journal eISSN: 2545-2835
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Language: English
Page range: 34 - 46
Published on: Oct 8, 2021
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year
Keywords:
Combustion chamber,
exit temperature pattern,
turbulent Schmidt number,
temperature dependence,
numerical simulation,
UDF,
ANSYS Fluent
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other,
Geosciences,
Geosciences, other,
Materials sciences,
Materials sciences, other,
Physics,
Physics, other

© 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.

Volume 2021 (2021): Issue 3 (September 2021)
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