THE HELICOPTER TURBOSHAFT ENGINE’S COMPUTER-INTEGRATED GAS TEMPERATURE IN FRONT OF THE COMPRESSOR TURBINE CONTROL SYSTEM

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Authors

Андрій Перекрест (ORCID: https://orcid.org/0000-0002-7728-9020)
Dmytro Shved (ORCID: https://orcid.org/0009-0005-4306-6805)
Mykola Guchenko (ORCID: https://orcid.org/0000-0002-9356-7414)
Sergei Osadchy (ORCID: https://orcid.org/0000-0002-1811-3594)
Nataliia Vladova (ORCID: https://orcid.org/0009-0009-7957-7497)

Publication Details

Journal: Electromechanical and energy saving systems
Published: 2025-01-01
DOI: https://doi.org/10.32782/2072-2052.2025.1.68.4
Primary Topic: Rocket and propulsion systems research
Type: article
Field-Weighted Citation Impact: 0.00

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article

THE HELICOPTER TURBOSHAFT ENGINE’S COMPUTER-INTEGRATED GAS TEMPERATURE IN FRONT OF THE COMPRESSOR TURBINE CONTROL SYSTEM

Андрій Перекрест, Dmytro Shved, Mykola Guchenko, Sergei Osadchy et al.

Jan 1, 2025

Electromechanical and energy saving systems

Rocket and propulsion systems research

article

THE HELICOPTER TURBOSHAFT ENGINE’S COMPUTER-INTEGRATED GAS TEMPERATURE IN FRONT OF THE COMPRESSOR TURBINE CONTROL SYSTEM

Андрій Перекрест, Dmytro Shved, Mykola Guchenko, Sergei Osadchy, Nataliia Vladova

January 1, 2025article en

Abstract

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Electromechanical and energy saving systems(1)

Affordable and clean energy

Openalex Percentile: Top 75%

Rocket and propulsion systems research

DOI Open Access PDF OpenAlex

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THE HELICOPTER TURBOSHAFT ENGINE’S COMPUTER-INTEGRATED GAS TEMPERATURE IN FRONT OF THE COMPRESSOR TURBINE CONTROL SYSTEM — Андрій Перекрест, Dmytro Shved, et al. · Electromechanical and energy saving systems (2025) | TGRS Research Map | TGRS