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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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| Main Authors: | , , , , |
|---|---|
| Formáid: | Artigo |
| Teanga: | Inglês |
| Foilsithe: |
Gdańsk University of Technology
2015-04-01
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| Sraith: | TASK Quarterly |
| Ábhair: | |
| Rochtain Ar Líne: | https://journal.mostwiedzy.pl/TASKQuarterly/article/view/1876 |
| Clibeanna: |
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