Experimental investigation of film cooling flow induced by shaped holes on a turbine blade

Annals of the New York Academy of Sciences

Volumn 934, Issue , 2001, Pages 313-320

  Barthet, S ^a   Bario, F ^a  

^a ECOLE CENTRALE DE LYON   (France)

Author keywords

[No Author keywords available]

Indexed keywords

CONFERENCE PAPER; COOLING; FILM; HYDRODYNAMICS; THERMAL ANALYSIS; TURBULENT FLOW; VELOCITY;

EID: 0034959350     PISSN: 00778923     EISSN: None     Source Type: Book Series    
DOI: 10.1111/j.1749-6632.2001.tb05865.x     Document Type: Conference Paper

References (11)

1. On the structure of jets in a crossflow
2. Effects of hole geometry and density on three-dimensional film cooling
3. Cooling jets and boundary layer interaction on the suction side of a turbine inlet guide vane
4. The laminar horseshoe vortex
5. Numerical investigation of film cooling flow induced by cylindrical and shaped holes