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Influence of the helicopter flight design speed on the selection of working process parameters for GTE

  • Aircraft and Rocket Engine Design and Development
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Abstract

This paper considers issues of designing a gas-turbine engine in the helicopter system at the early design stages. The optimum and rational values of engine working process parameters at different flight speeds of the flight vehicle (FV) are analyzed. Several characteristics of mathematical models (MM) that form the helicopter–engine system, are described.

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References

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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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Additional information

Original Russian Text © V.A. Grigor’ev, A.O. Zagrebel’nyi, 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2017, No. 2, pp. 50–54.

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Grigor’ev, V.A., Zagrebel’nyi, A.O. Influence of the helicopter flight design speed on the selection of working process parameters for GTE. Russ. Aeronaut. 60, 214–218 (2017). https://doi.org/10.3103/S1068799817020088

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  • DOI: https://doi.org/10.3103/S1068799817020088

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