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Russian Aeronautics

, Volume 61, Issue 3, pp 452–459 | Cite as

3D Investigations of the High Pressure Turbine Vane Platform Convection Cooling and Convection-Film Cooling

  • Yu. G. GorelovEmail author
  • V. V. Anan’ev
Aircraft and Rocket Engine Theory
  • 4 Downloads

Abstract

3D ANSYS CFX conjugate calculation was carried out to compare cooling effectiveness of the high pressure turbine vane platforms with the film cooling and the convection-film cooling.

Keywords

vane platform cooling effectiveness set of nozzles high pressure turbine gas turbine engine 

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Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  1. 1.Salyut Gas Turbine Engineering Research and Production CenterMoscowRussia

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