Special features of aerodynamic and thermal improvement of turbine nozzles for advanced gas turbine engines

V. A. Poletaev; A. E. Remizov; V. V. Vyatkov; V. V. Lebedev

doi:10.3103/S1068799816010141

Special features of aerodynamic and thermal improvement of turbine nozzles for advanced gas turbine engines

作者: Poletaev V.A.¹, Remizov A.E.¹, Vyatkov V.V.¹, Lebedev V.V.¹
隶属关系:
1. P.A. Solovyov Rybinsk State Aviation Technical University
期: 卷 59, 编号 1 (2016)
页面: 89-94
栏目: Aircraft and Rocket Engine Design and Development
URL: https://journals.rcsi.science/1068-7998/article/view/229586
DOI: https://doi.org/10.3103/S1068799816010141
ID: 229586

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详细

Some results of investigating the geometrical and jet impact on secondary flows and thermal state of cooled inter-profile end surfaces of gas turbine engine nozzles have been set forth under different secondary flows interaction degree in a blade channel.