Enviar artigo por via de e-mail Stability of Decisions in Choosing the Operating Parameter Values of the Gas Turbine Engine in the Helicopter System at the Initial Design Stage
- Autores: Grigor’ev V.1, Zagrebel’nyi A.1
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Afiliações:
- Samara University
- Edição: Volume 62, Nº 1 (2019)
- Páginas: 163-166
- Seção: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230886
- DOI: https://doi.org/10.3103/S1068799819010239
- ID: 230886
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Resumo
Mathematical models are obtained that make it possible to simplify the accounting for the uncertainties in the initial data values when designing a gas turbine engine in a helicopter system at the initial design stages.
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Sobre autores
V. Grigor’ev
Samara University
Email: zao_sam156@mail.ru
Rússia, Moskovskoe shosse 34, Samara, 443086
A. Zagrebel’nyi
Samara University
Autor responsável pela correspondência
Email: zao_sam156@mail.ru
Rússia, Moskovskoe shosse 34, Samara, 443086
