INFLUENCE OF AIR COOLING AND AIR-JET VORTEX GENERATOR ON FLOW STRUCTURE IN TURBINE PASSAGE

The paper concerns the experimental investigations and numerical simulations of a high loaded model of a turbine blade. An increase in the blade load leads to enlargement of a local supersonic zone terminated by a shock wave on the suction side. The Mach number upstream of the shock reaches up to 1...

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Bibliographic Details
Main Authors: RYSZARD SZWABA, PAWEŁ FLASZYŃSKI, JAN ARTUR SZUMSKI, PIOTR DOERFFER
Format: Article
Language:English
Published: Gdańsk University of Technology 2015-04-01
Series:TASK Quarterly
Subjects:
Online Access:https://journal.mostwiedzy.pl/TASKQuarterly/article/view/1881