Film cooling on a flat surface with a single row of cylindrical angled holes: Effect of discrete tabs

ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE)

Volumn 2000-U, Issue , 2000, Pages 3-12

  Ekkad, Srinath V ^a   Nasir, Hasan ^a   Acharya, Sumanta ^a  

^a Louisiana State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COOLING; FIGHTER AIRCRAFT; LIQUID CRYSTALS; WIND TUNNELS;

CYLINDRICAL HOLES; DOWN-STREAM; FILM COOLING; FILM COOLING PERFORMANCE; FLATTER SURFACES; FREESTREAM TURBULENCE; HOLE EFFECTS; LOW-SPEED WIND TUNNEL; STREAMWISE DIRECTIONS; TRANSIENT LIQUID CRYSTAL TECHNIQUE;

REYNOLDS NUMBER;

EID: 84994515010     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/IMECE2000-1455     Document Type: Conference Paper

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