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Simulation Model of a Propulsion System of a Supersonic Aircraft

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Russian Engineering Research Aims and scope

Abstract

A model is proposed for the propulsion system of a supersonic aircraft. The model is used for preliminary study of the outline and characteristics of aviation gas-turbine engines. It permits assessment of the propulsion system’s effective characteristics.

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Authors and Affiliations

  1. Moscow Aviation Institute, 125080, Moscow, Russia

    A. D. Alendar’ & M. V. Siluyanova

Authors
  1. A. D. Alendar’
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  2. M. V. Siluyanova
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Correspondence to A. D. Alendar’ or M. V. Siluyanova.

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Translated by B. Gilbert

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Alendar’, A.D., Siluyanova, M.V. Simulation Model of a Propulsion System of a Supersonic Aircraft. Russ. Engin. Res. 41, 676–679 (2021). https://doi.org/10.3103/S1068798X21070042

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  • DOI: https://doi.org/10.3103/S1068798X21070042

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