Systematic experimental and numerical investigations on the aerothermodynamics of a film cooled turbine cascade with variation of the cooling hole shape: Part i experimental approach

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2000, Pages

  Ganzert, Wolfgang ^a   Hildebrandt, Thomas ^b   Fottner, Leonhard ^a  

^a BUNDESWEHR UNIVERSITY MUNICH   (Germany)

^b NUMECA Ing Buro Th Hildebrandt   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; CASCADES (FLUID MECHANICS); COOLING; HEAT TRANSFER COEFFICIENTS; LIQUID CRYSTALS; REYNOLDS NUMBER; THERMODYNAMICS; TURBINES;

BOUNDARY LAYER DEVELOPMENT; EXPERIMENTAL APPROACHES; FILM COOLING CONFIGURATIONS; HEAT TRANSFER MEASUREMENTS; INLET TURBULENCE LEVELS; NUMERICAL INVESTIGATIONS; SURFACE HEAT TRANSFER; TOTAL PRESSURE LOSS COEFFICIENT;

HEAT TRANSFER;

EID: 84955165179     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0295     Document Type: Conference Paper

References (24)

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