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...

Volledige beschrijving

Bewaard in:
Bibliografische gegevens
Hoofdauteurs: PIOTR KACZYŃSKI, RYSZARD SZWABA, BARTOSZ PUCHOWSKI, PIOTR DOERFFER, PAWEŁ FLASZYŃSKI
Formaat: Artigo
Taal:Inglês
Gepubliceerd in: Gdańsk University of Technology 2015-04-01
Reeks:TASK Quarterly
Onderwerpen:
turbine blade
internal channel
radial passage
blade cooling
Online toegang:https://journal.mostwiedzy.pl/TASKQuarterly/article/view/1876
Tags: Voeg label toe
Geen labels, Wees de eerste die dit record labelt!

Gelijkaardige items