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

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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
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Header DbId: aci
DbLabel: Applied Science & Technology Source
An: 136165018
AccessLevel: 2
PubType: Academic Journal
PubTypeId: academicJournal
PreciseRelevancyScore: 0
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  Data: Investigation of the Trailing Edge Modification Effect on Compressor Blade Aerodynamics Using SST k-ω Turbulence Model.
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  Data: <searchLink fieldCode="JN" term="%22Aerospace+%28MDPI+Publishing%29%22">Aerospace (MDPI Publishing)</searchLink>; Apr2019, Vol. 6 Issue 4, p48, 1p
PLink https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&db=aci&AN=136165018
RecordInfo BibRecord:
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    Identifiers:
      – Type: doi
        Value: 10.3390/aerospace6040048
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      – Code: eng
        Text: English
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        StartPage: 48
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      – TitleFull: Investigation of the Trailing Edge Modification Effect on Compressor Blade Aerodynamics Using SST k-ω Turbulence Model.
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            NameFull: Kaewbumrung, Mongkol
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            NameFull: Tangsopa, Worapol
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              Text: Apr2019
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              Y: 2019
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