Method of computation of gas-tube engines in windmill modes
- 作者: Leshchenko I.A.1, Rozhkova M.V.2, Tarmaev A.A.2, Donskikh V.V.2
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隶属关系:
- PSC “UEC-Saturn”
- Moscow Aviation Institute
- 期: 卷 24, 编号 2 (2025)
- 页面: 48-60
- 栏目: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journal-vniispk.ru/2542-0453/article/view/311521
- DOI: https://doi.org/10.18287/2541-7533-2025-24-2-48-60
- ID: 311521
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Providing the restart capability of engine in flight is an important certification requirement applied to engine units of manned and unmanned aerial vehicles oriented to ensuring flight safety with a given level of technical characteristics. It is important to perform preliminary analysis and evaluation of gas turbine engine parameters at the start-up and windmill modes before rig and flight tests. The work presents a method for computation of the windmill modes of gas turbine engines based on the use of analytical and numerical methods. The Numeca Fine/Turbo software package was used to calculate the maps of turbomachines at the sub-idle modes. The solution of the system of nonlinear equations for computing the start-up and windmill modes is carried out using the combined Newton-Nelder-Mead method. The application of the method is demonstrated by a mixed flow two-shaft turbojet.
作者简介
I. Leshchenko
PSC “UEC-Saturn”
编辑信件的主要联系方式.
Email: igor.leshchenko@thermogte.ru
ORCID iD: 0000-0003-0231-8680
Doctor of Science (Engineering), Senior Researcher, Head of the Thermodynamics Team
俄罗斯联邦M. Rozhkova
Moscow Aviation Institute
Email: rozhkovamv@mai.ru
ORCID iD: 0009-0006-9650-3471
Postgraduate Student of the Department of Theory of Air-breathing Engines
俄罗斯联邦A. Tarmaev
Moscow Aviation Institute
Email: t38_69@mail.ru
ORCID iD: 0000-0002-4549-4169
Candidate of Science (Engineering), Associate Professor of the Department of Theory of Air-breathing Engines
俄罗斯联邦V. Donskikh
Moscow Aviation Institute
Email: vic@mai.ru
Director of the Center for Information Security, Senior Lecturer of the Department of Aerospace Thermal Engineering
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