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Transactions on Aerospace Research
Volume 2021 (2021): Issue 3 (September 2021)
Open Access
Numerical Simulation of the Exit Temperature Pattern of an Aircraft Engine Using a Temperature-Dependent Turbulent Schmidt Number
Igor F. Kravchenko
Igor F. Kravchenko
,
Dmytro V. Kozel
Dmytro V. Kozel
and
Serhii A. Yevsieiev
Serhii A. Yevsieiev
| Oct 08, 2021
Transactions on Aerospace Research
Volume 2021 (2021): Issue 3 (September 2021)
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Published Online:
Oct 08, 2021
Page range:
34 - 46
DOI:
https://doi.org/10.2478/tar-2021-0015
Keywords
Combustion chamber
,
exit temperature pattern
,
turbulent Schmidt number
,
temperature dependence
,
numerical simulation
,
UDF
,
ANSYS Fluent
© 2021 Igor F. Kravchenko et al., published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
Igor F. Kravchenko
SE “Ivchenko-Progress”
Zaporozhye, Ukraine
Dmytro V. Kozel
SE “Ivchenko-Progress”
Zaporozhye, Ukraine
Serhii A. Yevsieiev
SE “Ivchenko-Progress”
Zaporozhye, Ukraine