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http://dx.doi.org/10.5293/kfma.2013.16.6.019

Effect of Tip Gap Height on Heat/Mass Transfer over a Cavity Squealer Tip  

Kang, Dong Bum (Graduate School, Kumoh National Institute of technology)
Moon, Hyun Suk (Graduate School, Kumoh National Institute of technology)
Lee, Sang Woo (Department of Mechanical Engineering, Kumoh National Institute of technology)
Publication Information
Abstract
The effect of tip gap height on heat/mass transfer characteristics on the floor of cavity squealer tip has been investigated in a turbine cascade for power generation by employing the naphthalene sublimation technique. The squealer rim height is chosen to be an optimal one of $h_{st}/c$ = 5.51% for the tip gap height-to-chord ratios of h/c = 1.0, 2.0, 3.0 and 4.0%. The results show that heat transfer on the cavity floor is strongly dependent upon the behavior of the cavity flow falling down onto the floor. For lower h/c, the floor heat transfer is influenced by the tip leakage flow falling down along the inner face of the suction-side squealer, whereas the floor heat transfer for higher h/c is augmented mainly due to the impingement of leakage flow on the floor near the leading edge. Compared to the plane tip surface heat transfer, the cavity floor heat transfer is less influenced by h/c. For h/c = 1.0%, the average thermal load is as low as a half of the plane tip surface one, and the difference in the thermal load between the two cases tends to decrease with increasing h/c.
Keywords
Turbine rotor blade; Cavity squealer tip; Tip gap height; Heat transfer;
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1 Mayle, R. E., and Metzger, D. E., 1982, "Heat Transfer at the Tip of an Unshrouded Turbine Blade," Proceedings of 7th International Heat Transfer Conference, Vol. 3, pp. 87-92.
2 Chyu, M. K., Moon, H. K., and Metzger, D. E., 1989, "Heat Transfer in the Tip Region of Grooved Turbine Blades," ASME Journal of Turbomachinery, Vol. 111, pp. 131-138.   DOI   ScienceOn
3 Azad, Gm. S., Han, J.-C., Teng, S., and Boyle, R. J., 2000, "Heat Transfer and Pressure Distributions on a Gas Turbine Blade Tip," ASME Journal of Turbomachinery, Vol. 122, pp. 717-724.   DOI   ScienceOn
4 Azad, Gm. S., Han, J.-C., and Boyle, R. J., 2000, "Heat Transfer and Pressure Distributions on the Squealer Tip of a Gas Turbine Blade," ASME Journal of Turbomachinery, Vol. 122, pp. 725-732.   DOI   ScienceOn
5 Papa, M., Goldstein, R. J., and Gori, F., 2003, "Effect of Tip Geometry and Tip Clearance on the Mass/Heat Transfer From a Large-Scale Gas Turbine Blade," ASME Journal of Turbomachinery, Vol. 125, pp. 90-96.   DOI   ScienceOn
6 Nasir, H., Ekkad, S. V., Kontrovitz, D, M., Bunker, R. S., and Prakash, C., 2004, "Effect of Tip Gap and Squealer Geometry on Detailed Heat Transfer Measurements over a High Pressure Turbine Rotor Blade Tip," ASME Journal of Turbomachinery, Vol. 126, pp. 221-228.   DOI   ScienceOn
7 Lee, S. W. and Chae, B. J., 2008, "Effect of Squealer Rim Height on Aerodynamic Losses Downstream of a High-Turning Turbine Rotor Blade," Experimental Thermal and Fluid Science, pp. Vol. 32, 1440-1447.   DOI   ScienceOn
8 Goldstein, R. J. and Cho, H. H., 1995, "A Review of Mass Transfer Measurements Using Naphthalene Sublimation," Experimental Thermal and Fluid Science, Vol. 10, pp. 416-434.   DOI   ScienceOn
9 Abernethy, R. B., Benedict, R. P. and Dowdell, R. B., 1985, "ASME Measurement Uncertainty," ASME Journal of Fluids Engineering, Vol. 107, pp. 161-164.   DOI
10 Lee, S. W., Moon, H. S., and Lee, S. E., 2009, "Tip Gap Height Effects on Flow Structure and Heat/Mass transfer over Plane Tip of a High-Turning Turbine Rotor Blade," International Journal of Heat and Fluid Flow, Vol. 30, pp. 198-210.   DOI   ScienceOn