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Air-to-Air Heat Exchanger in a Turbofan Ramjet Engine

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Russian Engineering Research Aims and scope

Abstract

Simulation of the operation of an air-to-air heat exchanger in a hybrid turbofan ramjet engine is considered. A model determining the preliminary configuration of the heat exchanger is developed, taking account of the parameters specified for the engine. The influence of the engine on the basic characteristics of the air-to-air heat exchanger determines its profile.

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Authors and Affiliations

  1. Moscow Aviation Institute, Moscow, Russia

    M. V. Siluyanova, D. N. Kuritsyn & A. N. Grunin

  2. Baranov Central Institute of Aviation Motor Development, Moscow, Russia

    A. N. Grunin

Authors
  1. M. V. Siluyanova
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  2. D. N. Kuritsyn
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  3. A. N. Grunin
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Correspondence to M. V. Siluyanova.

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Translated by B. Gilbert

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Siluyanova, M.V., Kuritsyn, D.N. & Grunin, A.N. Air-to-Air Heat Exchanger in a Turbofan Ramjet Engine. Russ. Engin. Res. 42, 267–269 (2022). https://doi.org/10.3103/S1068798X22030212

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  • DOI: https://doi.org/10.3103/S1068798X22030212

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