An infrared technique for evaluating turbine airfoil cooling designs

Journal of Turbomachinery

Volumn 122, Issue 1, 2000, Pages 170-177

  Sweeney, P C ^a   Rhodes, J F ^b  

^a ROLLS ROYCE CORPORATION   (United States)

^b Allison Advanced Development Co   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BLOWING RATIO; COOLING AIR; COOLING DESIGNS; DESIGN CONCEPT; DESIGN FEATURES; EXPERIMENTAL APPROACHES; FILM COOLING HOLE; FILM HOLES; FLAT PLATE; FLAT PLATE SURFACE; FREE STREAM; INFRARED TECHNIQUE; INTERNAL COOLING; IR TEMPERATURE; IS COSTS; NON-INTRUSIVE; OVERALL COOLING EFFECTIVENESS; ROOM TEMPERATURE; SPATIAL RESOLUTION; STAGGERED ARRAYS; STEADY-STATE MEASUREMENTS; SURFACE TEMPERATURE MEASUREMENT; TEMPERATURE RATIO; TURBINE AIRFOILS; ZINC SELENIDE;

AIRFOILS; ATMOSPHERIC TEMPERATURE; COOLING; IMAGE RESOLUTION; INFRARED RADIATION; SURFACE PROPERTIES; TEMPERATURE MEASUREMENT; THERMOCOUPLES; TURBINE COMPONENTS;

DESIGN;

AEROFOIL; COOLING; GAS TURBINE;

EID: 0034069824     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.555438     Document Type: Article

References (15)

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