Calculation of flow characteristics of liquid fuel supplied through pressure jet atomizers of small-sized gas turbine engines
- Authors: Gurakov N.I.1, Zubrilin I.A.1, Hernandez Morales M.1, Yakushkin D.V.1, Didenko A.A.1, Matveev S.G.1, Komisar Y.V.1
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Affiliations:
- Samara National Research University
- Issue: Vol 20, No 2 (2021)
- Pages: 19-35
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/8927
- DOI: https://doi.org/10.18287/2541-7533-2021-20-2-19-35
- ID: 8927
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Full Text
Abstract
The paper presents the results of studying the flow characteristics of liquid fuel in pressure jet atomizers of small-sized gas turbine engines with nozzle diameters of 0.4-0.6 mm for various operating and design parameters. The study was carried out using experimental measurements, semi-empirical correlations and CFD (computational fluid dynamics) methods. The Euler approach, the volume- of- fluid (VOF) method, was used to model multiphase flows in CFD simulations. Good agreement was obtained between experimental and predicted data on the fuel coefficient and the primary spray cone angle at the nozzle outlet. Besides, the assessment of the applicability of semi-empirical techniques for the nozzle configurations under consideration is given. In the future, the flow characteristics in question (the nozzle flow rate, the fuel film thickness, and the primary spray cone angle) can be used to determine the mean diameter of the droplets (SMD) required to fully determine the boundary conditions of fuel injection when modeling combustion processes in combustion chambers of small-sized gas turbine engines.
About the authors
N. I. Gurakov
Samara National Research University
Author for correspondence.
Email: nikgurakov@gmail.com
ORCID iD: 0000-0003-4217-0879
Postgraduate Student of the Department of Thermal Engineering and Thermal Engines
Russian FederationI. A. Zubrilin
Samara National Research University
Email: zubrilin.ia@ssau.ru
ORCID iD: 0000-0001-5876-8571
Candidate of Science (Engineering), Associate Professor of the Department of Thermal Engineering and Thermal Engines
Russian FederationM. Hernandez Morales
Samara National Research University
Email: mariohernandezmo_4_2@hotmail.com
ORCID iD: 0000-0002-0592-0530
Postgraduate Student of the Department of Thermal Engineering and Thermal Engines
Russian FederationD. V. Yakushkin
Samara National Research University
Email: yakushkindv@gmail.com
Student
Russian FederationA. A. Didenko
Samara National Research University
Email: aanm_didenko@rambler.ru
Candidate of Science (Engineering), Associate Professor of the Department of Thermal Engineering and Thermal Engines
Russian FederationS. G. Matveev
Samara National Research University
Email: msg@ssau.ru
Candidate of Science (Engineering), Professor of the Department of Thermal Engineering and Thermal Engines
Russian FederationYu. V. Komisar
Samara National Research University
Email: komisar.yuv@ssau.ru
Design Engineer of the Department of Aircraft Engine Theory
Russian FederationReferences
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