A numerical study on flow and heat transfer characteristics of film cooling with a compound angle hole

KSME International Journal

Volumn 12, Issue 5, 1998, Pages 963-971

  Lee, Jung Hee ^a  

^a Chung Ang University College of Medicine   (South Korea)

Author keywords

Film Cooling; Film Cooling Effectiveness; Finite Volume Method; Longitudinal Skin Friction; Longitudinal Vortex; Skew Angle

Indexed keywords

EID: 0006525537     PISSN: 12264865     EISSN: None     Source Type: Journal    
DOI: 10.1007/BF02945563     Document Type: Article

References (5)

1. Compton, D. A. and Johnston, J. P., 1992, "Streamwise Vortex Production by Pitched and Skewed Jets in a Turbulent Boundary Layer," AIAA Journal, Vol. 30, No. 3, pp. 640-647.
2. Goldstein, R. J., Eckert, E. R. G., and Ramsey, J. W., 1970, "Film Cooling Following Inj ection Through Inclined Circular Tubes," Israel Journal of Technology, Vol. 8, pp. 584-588.
3. Honami, S., Shizawa, T. and Uchiyama, A., 1994, "Behavior of the Laterally Injected Jet in Film Cooling: Measurements of Surface Temperature and Velocity Temperature Field within the Jet," ASME J. of Turbomachinery, Vol. 116, pp. 106-112.
4. Lee, S. W., Kim, Y. B. and Lee, J. S., 1997, "Flow Characteristics and Aerodynamic Losses of Film-Cooling Jets with Compound Angle Orientations," ASME J. of Turbomachinery, Vol. 119, pp. 310-319.
5. Leylek, J. H. and Zerkle, R. D., 1994, "Discrete -Jet Film Cooling: A Comparison of Computational Results with Experiments," ASME J. of Turbomachinery, Vol. 116, pp. 358 -368.