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Optimal distribution of turboprop engine free energy between the screw and the jet with mass characteristics taken into account
- Authors: Grigoriev V.A.1, Prokaev A.S.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 12, No 3-2 (2013): Vestnik SSAU
- Pages: 88-92
- Section: ISSUE WITHOUT SECTION
- URL: https://journals.ssau.ru/vestnik/article/view/1827
- DOI: https://doi.org/10.18287/1998-6629-2013-0-3-2(41)-88-92
- ID: 1827
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Abstract
The paper presents an analysis of research in optimal distribution of the airscrew thrust and the jet thrust of the turboprop engine. A conclusion is made as to the necessity of evaluating the efficiency of the power plant being a part of the aircraft.
About the authors
V. A. Grigoriev
Samara State Aerospace University
Author for correspondence.
Email: va_grig@ssau.ru
Doctor of Sciences (Engineering)
Professor of the Aircraft Engine Theory Department
Russian FederationA. S. Prokaev
Samara State Aerospace University
Email: prok.alexey@mail.ru
Postgraduate Student of the Aircraft Engine Theory Department
Russian FederationReferences
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- Григорьев, В.А. Универсальная учебная установка с малоразмерными ГТД [Текст] / В.А. Григорьев // Тр. КуАИ. Вып. 57. - Куйбышев, 1972. - С. 87-93.
- Теория воздушно-реактивных двигателей [Текст] / под ред. д-ра техн. наук С.М. Шляхтенко. - М.: Машиностроение, 1975. - 568 с.
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