A detailed analysis of film cooling physics: Part IV- Compound-angle injection with shaped holes

Journal of Turbomachinery

Volumn 122, Issue 1, 2000, Pages 133-145

  Brittingham, R A ^a   Leylek, J H ^a  

^a AMRL   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADIABATIC EFFECTIVENESS; BLOWING RATIO; COMBINED EFFECT; COMPOUND ANGLE; COMPUTATIONAL METHODOLOGY; CONVERGENCE ACCELERATORS; CROSS FLOWS; CYLINDRICAL HOLES; DENSITY RATIO; DOMINANT MECHANISM; EXIT PLANES; EXPERIMENTAL DATA; FILM COOLING; FLAT PLATE; FLOW PHYSICS; GEOMETRIC CONFIGURATIONS; LENGTH TO DIAMETER RATIO; MULTI-GRID; MULTIBLOCKS; NAVIER-STOKES CODE; PITCH-TO-DIAMETER RATIOS; SHAPED HOLES; SURFACE DATA; TURBINE PARAMETERS; UNDERRELAXATION;

COOLING; REYNOLDS NUMBER;

FLOW FIELDS;

COOLING; FILM; GAS TURBINE; MATHEMATICAL MODELING;

EID: 0034108018     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.555419     Document Type: Article

References (16)

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