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

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Bibliographic Details
Title: Investigation of the Trailing Edge Modification Effect on Compressor Blade Aerodynamics Using SST k-ω Turbulence Model.
Authors: Kaewbumrung, Mongkol1,2, mongkol.kaewbumrung@gmail.comworapol.plz@gmail.com, Tangsopa, Worapol2, Thongsri, Jatuporn2, jatuporn.th@kmitl.ac.th
Source: Aerospace (MDPI Publishing); Apr2019, Vol. 6 Issue 4, p48, 1p
Database: Applied Science & Technology Source
Description
ISSN:22264310
DOI:10.3390/aerospace6040048