Film-cooling effectiveness on a gas turbine blade tip using pressure sensitive paint

Proceedings of the ASME Turbo Expo 2004

Volumn 3, Issue , 2004, Pages 241-250

  Ahn, Jaeyong ^a   Mhetras, Shantanu ^a   Han, Je Chin ^a  

^a Texas AandM University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR; COOLING; FILMS; GAS TURBINES; MASS TRANSFER; NITROGEN; OXYGEN; PAINT; REYNOLDS NUMBER; TURBULENCE;

FILM-COOLING EFFECTIVENESS; SQUEALER; SURFACE STATIC PRESSURE;

TURBOMACHINE BLADES;

EID: 10244252781     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/gt2004-53249     Document Type: Conference Paper

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