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Stability of Decisions in Choosing the Operating Parameter Values of the Gas Turbine Engine in the Helicopter System at the Initial Design Stage

  • Aircraft and Rocket Engine Design and Development
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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.

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Authors and Affiliations

  1. Samara University, Moskovskoe shosse 34, Samara, 443086, Russia

    V. A. Grigor’ev & A. O. Zagrebel’nyi

Authors
  1. V. A. Grigor’ev
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  2. A. O. Zagrebel’nyi
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Correspondence to A. O. Zagrebel’nyi.

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Grigor’ev, V.A., Zagrebel’nyi, A.O. Stability of Decisions in Choosing the Operating Parameter Values of the Gas Turbine Engine in the Helicopter System at the Initial Design Stage. Russ. Aeronaut. 62, 163–166 (2019). https://doi.org/10.3103/S1068799819010239

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  • DOI: https://doi.org/10.3103/S1068799819010239

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