Investigation of the Trailing Edge Modification Effect on...

Aerospace 2019 / 04 Vol. 6; Iss. 4

Investigation of the Trailing Edge Modification Effect on Compressor Blade Aerodynamics Using SST k-ω Turbulence Model

Kaewbumrung,, Tangsopa,, Thongsri,
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Volume:
6
Language:
english
Journal:
Aerospace
DOI:
10.3390/aerospace6040048
Date:
April, 2019
File:
PDF, 5.50 MB
english, 2019
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