Han, J. C., Dutta, S., and Ekkad, S. V., 2000, Gas Turbine Heat Transfer and Cooling Technology, Taylor & Francis, New York
Metzger,
D. E., Bunker,
R. S., and Chyu,
M. K., 1989, “Cavity Heat Transfer on a Transverse Grooved Wall in a Narrow Flow Channel,” ASME J. Heat Transfer, 111, pp. 73–79.
Chyu,
M. K., Moon,
H. K., and Metzger,
D. E., 1989, “Heat Transfer in the Tip Region of Grooved Turbine Blades,” ASME J. Turbomach., 111, pp. 131–138.
Heyes, F. J. G., Hodson, H. P., and Dailey, G. M., 1991, “The Effect of Blade Tip Geometry on the Tip Leakage Flow in Axial Turbine Cascades,” ASME Paper No. 91-GT-135.
Yang, T. T., and Diller, T. E., 1995, “Heat Transfer and Flow for a Grooved Turbine Blade Tip in a Transonic Cascade,” ASME-95-WA/HT-29.
Ameri, A. A., Steinthorsson, E., and Rigby, L. David, 1997, “Effect of Squealer Tip on Rotor Heat Transfer and Efficiency,” ASME Paper No. 97-GT-128.
Dunn,
M. G., and Haldeman,
C. W., 2000, “Time-Averaged Heat Flux for a Recessed Tip, Lip, and Platform of a Transonic Turbine Blade,” ASME J. Turbomach., 122, pp. 692–697.
Azad,
G. M. S., Han,
J. C., Teng,
S., and Boyle,
R., 2000, “Heat Transfer and Pressure Distributions on a Gas Turbine Blade Tip,” ASME J. Turbomach., 122, pp. 717–724.
Azad,
G. M. S., Han,
J. C., and Boyle,
R., 2000, “Heat Transfer and Pressure Distributions on the Squealer Tip of a Gas Turbine Blade,” ASME J. Turbomach., 122, pp. 725–732.
Azad,
G. M. S., Han,
J. C., Bunker,
R. S., and Lee,
C. P., 2002, “Effect of Squealer Geometry Arrangement on a Gas Turbine Blade Tip Heat Transfer,” ASME J. Heat Transfer, 124, pp. 452–459.
Mayle, R. E., and Metzger, D. E., 1982, “Heat Transfer at the Tip of an Unshrouded Turbine Blade,” Proc. Seventh Int. Heat Transfer Conf., Hemisphere Pub., pp. 87–92.
Metzger,
D. E., and Rued,
K., 1989, “The Influence of Turbine Clearance Gap Leakage on Passage Velocity and Heat Transfer Near Blade Tips. Part I: Sink Flow Effects on Blade Pressure Side,” ASME J. Turbomach., 111, pp. 284–292.
Rued,
K., and Metzger,
D. E., 1989, “The Influence of Turbine Clearance Gap Leakage on Passage Velocity and Heat Transfer Near Blade Tips. Part II: Source Flow Effects on Blade Pressure Side,” ASME J. Turbomach., 111, pp. 293–300.
Metzger,
D. E., Dunn,
M. G., and Hah,
C., 1991, “Turbine Tip and Shroud Heat Transfer,” ASME J. Turbomach., 113, pp. 502–507.
Bunker,
R. S., Baily,
J. C., and Ameri,
A. A., 2000, “Heat Transfer and Flow on the First Stage Blade Tip of a Power Generation Gas Turbine: Part 1: Experimental Results,” ASME J. Turbomach., 122, pp. 272–277.
Bunker, R. S., and Baily, J. C., 2001, “Effect of Squealer Cavity Depth and Oxidation on Turbine Blade Tip Heat Transfer,” ASME Paper No. 2001-GT-0155.
Teng,
S., Han,
J. C., and Azad,
G. M. S., 2001, “Derailed Heat Transfer Coefficient Distributions on a Large-Scale Gas Turbine Blade Tip,” ASME J. Heat Transfer, 123, pp. 803–809.
Ameri, A. A., and Steinthorsson, E., 1995, “Prediction of Unshrouded Rotor Blade Tip Heat Transfer,” ASME Paper No. 95-GT-142.
Ameri, A. A., and Steinthorsson, E., 1996, “Analysis of Gas Turbine Rotor Blade Tip and Shroud Heat Transfer,” ASME Paper No. 96-GT-189.
Ameri,
A. A., Steinthorsson,
E., and Rigby,
L. David, 1999, “Effects of Tip Clearance and Casing Recess on Heat Transfer and Stage Efficiency in Axial Turbines,” ASME J. Turbomach., 121, pp. 683–693.
Ameri,
A. A., and Bunker,
R. S., 2000, “Heat Transfer and Flow on the First Stage Blade Tip of a Power Generation Gas Turbine: Part 2: Simulation Results,” ASME J. Turbomach., 122, pp. 272–277.
Ameri, A. A., and Rigby, D. L., 1999, “A Numerical Analysis of Heat Transfer and Effectiveness on Film Cooled Turbine Blade Tip Models,” NASA/CR 1999-209165.
Ameri,
A. A., 2001, “Heat Transfer and Flow on the Blade Tip of a Gas Turbine Equipped With a Mean-Camberline Strip,” ASME J. Turbomach., 123, pp. 704–708.
Rhee, D. H., Choi, J. H., and Cho, H. H., 2001, “Effect of Blade Tip Clearance on Turbine Shroud Heat/Mass Transfer,” ASME Paper No. 2001-GT-0158.
Jin, P., and Goldstein, R. J., 2002, “Local Mass/Heat Transfer on a Turbine Blade Tip,” The 9th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, February 10–14, HT-ABS-012, pp. 1–11.
Jin, P., and Goldstein, R. J., 2002, “Local Mass/Heat Transfer on Turbine Blade Near-Tip Surfaces,” ASME Paper No. GT-2002-30556.
Papa, M., Goldstein, R. J., and Gori, F., 2002, “Effects of Tip Geometry and Tip Clearance on the Mass/Heat Transfer From a Large-Scale Gas Turbine Blade,” ASME Paper No. GT-2002-30192.
Kwak, J. S., and Han, J. C., 2003, “Heat Transfer Coefficient on a Gas Turbine Blade Tip and Near Tip Regions,” presented at the 8th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, St. Louis, June, Paper No. AIAA-2002-3012; Also, AIAA J. Thermophysics and Heat Transfer, 17 (3).
Kline,
S. J., and McClintock,
F. A., 1953, “Describing Uncertainties in Single Sample Experiments,” Mech. Eng. (Am. Soc. Mech. Eng.), 75, pp. 3–8.
