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Special features of aerodynamic and thermal improvement of turbine nozzles for advanced gas turbine engines |
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| Authors: | V A Poletaev A E Remizov V V Vyatkov V V Lebedev |
| Abstract: | 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. |
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