Thermal Engineering

, Volume 65, Issue 13, pp 1024–1028 | Cite as

About Calculation of Combined Cooling Systems for Propulsion Engines

  • D. M. BorisovEmail author
  • Y. A. Shuraev
  • V. V. Mironov


A numerical method is proposed for solving conjugate heat transfer problems as applied for calculation of combined cooling systems for combustion chambers of propulsion systems. A procedure is presented for joint calculation of temperature conditions of gaseous cooling film and cooling system elements in the entire cross-section of a combustion chamber, including the inner wall material. The numerical results and their verification are presented.


propulsion systems gaseous cooling film combustion chambers combined cooling conjugate heat transfer 


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Copyright information

© Pleiades Publishing, Inc. 2018

Authors and Affiliations

  • D. M. Borisov
    • 1
    Email author
  • Y. A. Shuraev
    • 1
  • V. V. Mironov
    • 1
  1. 1.Federal State Unitary Enterprise State Scientific Center Keldysh Research CenterMoscowRussia

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