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AERODYNAMIC ENHANCEMENT IN INNER CHANNEL OF TURBINE BLADE

This paper presents the numerical and experimental study of the flow structure in a radial cooling passage model of a gas turbine blade. The investigations focus on the flow aerodynamics in the channel, which is an accurate representation of the configuration used in aero engines. The flow structur...

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Wedi'i Gadw mewn:
Manylion Llyfryddiaeth
Prif Awduron: PIOTR KACZYŃSKI, RYSZARD SZWABA, BARTOSZ PUCHOWSKI, PIOTR DOERFFER, PAWEŁ FLASZYŃSKI
Fformat: Artigo
Iaith:Inglês
Cyhoeddwyd: Gdańsk University of Technology 2015-04-01
Cyfres:TASK Quarterly
Pynciau:
Mynediad Ar-lein:https://journal.mostwiedzy.pl/TASKQuarterly/article/view/1876
Tagiau: Ychwanegu Tag
Dim Tagiau, Byddwch y cyntaf i dagio'r cofnod hwn!