Bunker, R., 2006, “Axial Turbine Blade Tips: Function, Design, and Durability,” J. Propul. Power, 22 (2), pp. 271–285.
Kim, Y. W., and Metzger, D. E., 1995, “Heat Transfer and Effectiveness on Film Cooled Turbine Blade Tip Model,” ASME J. Turbomach.
[CrossRef], 117 , pp. 12–21.
Kim, Y. W., Downs, J. P., Soechting, F. O., Abdel-Messeh, W., Steuber, G. D., and Tanrikut, S., 1995, “A Summary of the Cooled Turbine Blade Tip Heat Transfer and Film Effectiveness Investigations Performed by Dr. D. E. Metzger,” ASME J. Turbomach.
[CrossRef], 117 , pp. 1–11.
Kwak, J. S., and Han, J. C., 2002, “Heat Transfer Coefficient and Film-Cooling Effectiveness on a Gas Turbine Blade Tip,” ASME Paper No. GT-2002-30194.
Kwak, J. S., and Han, J. C., 2002, “Heat Transfer Coefficient and Film-Cooling Effectiveness on the Squealer Tip of a Gas Turbine Blade,” ASME Paper No. GT-2002-30555.
Ahn, J., Mhetras, S. P., and Han, J. C., 2004, “Film-Cooling Effectiveness on a Gas Turbine Blade Tip,” ASME Paper No. GT-2004-53249.
Christophel, J. R., Thole, K. A., and Cunha, F. J., 2004, “Cooling the Tip of a Turbine Blade Using Pressure Side Holes, Part I: Adiabatic Effectiveness Measurements,” ASME Paper No. GT-2004-53249.
Christophel, J. R., Thole, K. A., and Cunha, F. J., 2004, “Cooling the Tip of a Turbine Blade Using Pressure Side Holes, Part II: Heat Transfer Measurements,” ASME Paper No. GT-2004-53254.
Mhetras, S. H., Yang, H., Gao, Z., and Han, J., 2006, “Film-Cooling Effectiveness on Squealer Cavity and Rim Walls of Gas-Turbine Blade Tip,” J. Propul. Power, 22 (4), pp. 889–899.
Mhetras, S., Narzary, D., Gao, Z., and Han, J., 2006, “Effect of a Cutback Squealer and Cavity Depth on Film Cooling Effectiveness for a Gas Turbine Blade Tip,” AIAA Paper No. 2006-3404.
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 I: Experimental Results,” ASME J. Turbomach.
[CrossRef], 122 , pp. 263–271.
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.
[CrossRef], 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.
[CrossRef], 122 , pp. 725–732.
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.
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
[CrossRef], 124 , pp. 452–459.
Kwak, J. S., Ahn, J., Han, J. C., Pang Lee, C., Bunker, R. S., Boyle, R., and Gaugler, R., 2002, “Heat Transfer Coefficients on Squealer Tip and Near Tip Regions of a Gas Turbine Blade With Single or Double Squealer,” ASME Paper No. GT-2003-38907.
Kwak, J. S., and Han, J. C., 2003, “Heat Transfer Coefficient on a Gas Turbine Blade Tip and Near Tip Regions,” J. Thermophys. Heat Transfer, 17 (3), pp. 297–303.
Kwak, J. S., and Han, J. C., 2003, “Heat Transfer Coefficient on the Squealer Tip and Near Squealer Tip Regions of a Gas Turbine Blade,” ASME J. Heat Transfer
[CrossRef], 125 , pp. 669–677.
Ameri, A. A., Steinthorsson, E., and Rigby, L. D., 1999, “Effects of Tip Clearance and Casing Recess on Heat Transfer and Stage Efficiency in Axial Turbines,” ASME J. Turbomach.
[CrossRef], 121 , pp. 683–693.
Ameri, A. A., and Rigby, D. L., 1999, “A Numerical Analysis of Heat Transfer and Effectiveness on Film Cooled Turbine Blade Tip Models,” NASA Technical Report No. CR-1999-209165.
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 II: Simulation Results,” ASME J. Turbomach.
[CrossRef], 122 , pp. 272–277.
Yang, H., Chen, H. C., and Han, J. C., 2004, “Numerical Prediction of Film Cooling and Heat Transfer With Different Film Hole Arrangements on the Plane and Squealer Tip of a Gas Turbine Blade,” ASME Paper No. 2004-GT-53199.
Metzger, D. E., Dunn, M. G., and Hah, C., 1991, “Turbine Tip and Shroud Heat Transfer,” ASME J. Turbomach.
[CrossRef], 113 , pp. 502–507.
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.
[CrossRef], 122 , pp. 692–697.
Rhee, D., and Cho, H., 2006, “Local Heat/Mass Transfer Characteristics on a Rotating Blade With Flat Tip in Low-Speed Annular Cascade, Part I: Near Tip Surface,” ASME J. Turbomach.
[CrossRef], 128 , pp. 96–109.
Rhee, D., and Cho, H., 2006, “Local Heat/Mass Transfer Characteristics on a Rotating Blade With Flat Tip in Low-Speed Annular Cascade, Part II: Tip and Shroud,” ASME J. Turbomach.
[CrossRef], 128 , pp. 110–119.
Halila, E. E., Lenahan, D. T., and Thomas, T. T., 1982, “Energy Efficient Engine,” General Electric Company, NASA, Report No. CR-167955.
Wright, L. M., Gao, Z., Varvel, T. A., and Han, J. C., 2005, “Assessment of Steady State PSP, TSP and IR Measurement Techniques for Flat Plate Film Cooling,” ASME Paper No. HT-2005-72363.
Coleman, H. W., and Steele, W. G., 1989, "Experimentation and Uncertainty Analysis for Engineers", Wiley, New York.
Gritsch, M., Schulz, A., and Wittig, S., 1997, “Discharge Coefficient Measurements of Film-Cooling Holes With Expanded Exits,” ASME Paper No. 97-GT-165.
