Email this article Stability of Decisions in Choosing the Operating Parameter Values of the Gas Turbine Engine in the Helicopter System at the Initial Design Stage
- Authors: Grigor’ev V.A.1, Zagrebel’nyi A.O.1
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Affiliations:
- Samara University
- Issue: Vol 62, No 1 (2019)
- Pages: 163-166
- Section: 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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Abstract
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.
About the authors
V. A. Grigor’ev
Samara University
Email: zao_sam156@mail.ru
Russian Federation, Moskovskoe shosse 34, Samara, 443086
A. O. Zagrebel’nyi
Samara University
Author for correspondence.
Email: zao_sam156@mail.ru
Russian Federation, Moskovskoe shosse 34, Samara, 443086
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