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


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.


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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