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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Autors principals: PIOTR KACZYŃSKI, RYSZARD SZWABA, BARTOSZ PUCHOWSKI, PIOTR DOERFFER, PAWEŁ FLASZYŃSKI
Format: Artigo
Idioma:Inglês
Publicat: Gdańsk University of Technology 2015-04-01
Col·lecció:TASK Quarterly
Matèries:
turbine blade
internal channel
radial passage
blade cooling
Accés en línia:https://journal.mostwiedzy.pl/TASKQuarterly/article/view/1876
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