3D investigation of heat exchange and hydrodynamics of high pressure turbine nozzle block platforms with different cooling schemes

Autor: Yu. G. Gorelov, V. V. Ananyev, D. A. Zolotuhina

Publikováno v: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 21, Iss 2, Pp 16-27 (2022)

Turbine nozzle blocks were tested and, as a result, problems of nozzle block lower platform alligatoring were detected. In the course of the research possible variants of cooling high pressure turbine nozzle block vane platforms were investigated. Ac

Externí odkaz: https://doaj.org/article/b19436c9993648899ade200453edeacc