Method of computation of gas-tube engines in windmill modes


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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

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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

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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

俄罗斯联邦

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