Film cooling on a modern HP turbine blade: Part III: Axial shaped holes

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

Volumn 3 B, Issue , 2002, Pages 953-959

  Ferguson, Jeffrey D ^a   Leylek, James H ^a   Buck, Frederick A ^b  

^a Clemson University   (United States)

^b GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL SHAPED HOLES; BLOWING RATIO; FILM COOLING; HOLE SHAPING;

COMPUTATIONAL FLUID DYNAMICS; COOLANTS; DENSITY OF LIQUIDS; PRESSURE EFFECTS; TURBOMACHINE BLADES; TURBULENCE;

GAS TURBINES;

EID: 0036994399     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30522     Document Type: Conference Paper

References (5)

1. Ferguson, J., Walters, D., and Leylek, J., 1998, "Performance of Turbulence Models and Near-Wall Treatments in Discrete-Jet Film-Cooling Simulations," ASME Paper No. 98-GT-438.
2. Fluent, Inc., 1997, Fluent 5 Users Manual, Lebanon, NH.
3. 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.
4. McGrath, E., and Leylek, J., 1999, "Physics of Hot Crossflow Ingestion in Film Cooling," Journal of Turbomachinery, Vol. 121, pp. 1-10.
5. Walters, D., and Leylek, J., 1997, "A Systematic Computational Methodology Applied to a Three-Dimensional Film-Cooling Flowfield," Journal of Turbomachinery, Vol. 119, pp. 777-785.