Heat Transfer Predictions in Aircraft Engines Combustors and Reheats

  • M. Desaulty
  • S. Meunier
Conference paper
Part of the EUROTHERM Seminars book series (EUROTHERM, volume 17)

Abstract

To cope with the important thermal fluxes which are met in aeronautical combustors, efficient cooling technologies are to be used. In order to calculate the thermal behavior, several methods are available at SNECMA.

As aerodynamics is very complex a satisfactory prediction of the wail temperatures is obtained by wall thermal calculations using boundary conditions coming from 2D or 3D Navier-Stokes calculation of the aerothermal field.

Keywords

Combustion Convection Liner Emissivity 

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References

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Copyright information

© Springer-Verlag Berlin, Heidelberg 1991

Authors and Affiliations

  • M. Desaulty
    • 1
  • S. Meunier
    • 1
  1. 1.Combustion DepartmentSNECMAMoissy CramayelFrance

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