Film cooling on a modern HP turbine blade: Part IV: Compound-angle shaped holes

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 3 B, Issue , 2002, Pages 945-952

  McGrath, E Lee ^a   Leylek, James H ^a   Buck, Frederick A ^b  

^a South   (United States)

^b GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FILM COOLING; HIGH PRESSURE TURBINE AIRFOIL; HOT CROSSFLOW;

AIRFOILS; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; COOLING SYSTEMS; INGESTION (ENGINES); VORTEX FLOW;

TURBOMACHINE BLADES;

EID: 0036991651     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30521     Document Type: Conference Paper

References (2)

1. Leylek, J., and Zerkle, R., 1994, "Discrete-Jet Film Cooling: A Comparison of Computational Results with Experiments," Journal of Turbomachinery, Vol. 116, pp. 358-368.
2. McGrath, E. L., and Leylek, J., 1999, "Physics of Hot Crossflow Ingestion in Film Cooling," Journal of Turbomachinery, Vol. 121, pp. 1-10.