Adiabatic effectiveness, thermal fields, and velocity fields for film cooling with large angle injection

Journal of Turbomachinery

Volumn 119, Issue 2, 1997, Pages 352-358

  Kohli, A ^a   Bogard, D G ^a  

^a The University of Texas at Austin   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0031496393     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841118     Document Type: Article

References (7)

1. Foster, N. W., and Lampard, D., 1980, “The Flow and Film Cooling Effectiveness Following Injection Through a Row of Holes,” ASME Journal of Engineering for Power, Vol 102, pp. 584-588.
2. Pedersen, D. R., Eckert, E. R. G., and Goldstein, R. J., 1977, “Film Cooling With Large Density Differences Between the Mainstream and the Secondary Fluid Measured by the Heat-Mass Transfer Analogy,” ASME Journal of Heat Transfer, Vol. 99, pp. 620-627.
3. Pietrzyk, J. R., 1989, “Experimental Study of the Interaction of Dense Jets with a Crossflow for Gas Turbine Applications,” Ph. D Thesis, University of Texas at Austin.
4. Pietrzyk, J. R., Bogard, D. G., and Crawford, M. E., 1990, “Effects of Density Ratio on the Hydrodynamics of Film Cooling,” ASME Journal of Turbomachinery, Vol. 112, pp. 437-443.
5. Schmidt, D. L., Sen, B., and Bogard, D. G., 1996, “Film Cooling With Compound Angle Holes: Adiabatic Effectiveness,” ASME Journal of Turbomachinery, Vol. 118, pp. 807-813.
6. Sinha, A. K., Bogard, D. G., and Crawford, M. E., 1991, “Film Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio,” ASME Journal of Turbomachinery, Vol. 113, pp. 442-449.
7. Thole, K. A., Sinha, A. K., Bogard, D. G., and Crawford, M. E., 1992, “Mean Temperature Measurements of Jets With a Crossflow for Gas Turbine Film Cooling Application,” in: Rotating Machinery Transport Phenomena, J. H. Kim and W. J. Yang, eds., Hemisphere Pub. Corp., New York.