Owen, J. M., 1988, “Air-Cooled Gas-Turbine Discs: A Review of Recent Research,” Int. J. Heat Fluid Flow, 9, pp. 354–365.
[CrossRef]Blair, M. F., 1974, “An Experimental Study of Heat Transfer and Film Cooling on Large-Scale Turbine Endwalls,” ASME J. Heat Transfer, 96, pp. 524–529.
[CrossRef]Roy, R. P., Squires, K. D., Gerendas, M., Song, S., Howe, W. J., and Ansari, A., 2000, “Flow and Heat Transfer at the Hub Endwall of Inlet Vane Passages—Experiments and Simulations,” ASME Paper No. 2000-GT-198.
Burd, S. W., and Simon, T. W., 2000, “Effects of Slot Bleed Injection Over a Contoured End Wall on Nozzle Guide Vane Cooling Performance: Part I—Flow Field Measurements,” ASME Paper No. 2000-GT-199.
Burd, S. W., Satterness, C. J., and Simon, T. W., 2000, “Effects of Slot Bleed Injection Over a Contoured End Wall on Nozzle Guide Vane Cooling Performance: Part II—Thermal Measurements,” ASME Paper No. 2000-GT-200.
Oke, R. A., Simon, T. W., Burd, S. W., and Vahlberg, R., 2000, “Measurements in a Turbine Cascade Over a Contoured Endwall: Discrete Hole Injection of Bleed Flow,” ASME Paper No. 2000-GT-214.
Kost, F., and Nicklas, M., 2001, “Film-Cooled Turbine Endwall in a Transonic Flow Field: Part I—Aero-Dynamic Measurements,” ASME Paper No. 2001-GT-0145.
Nicklas, M., 2001, “Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II—Heat Transfer and Film-Cooling Effectiveness,” ASME Paper No. 2001-GT-0146.
Oke, R. A., and Simon, T. W., 2002, “Film Cooling Experiments With Flow Introduced Upstream of a First Stage Nozzle Guide Vane Through Slots of Various Geometries,” ASME Paper No. GT2002-30169.
[CrossRef]Thole, K. A., and Knost, D. G., 2005, “Heat Transfer and Film Cooling for the Endwall of a First Stage Turbine Vane,” Int. J. Heat Mass Transfer, 48, pp. 5255–5269.
[CrossRef]Knost, D. G., and Thole, K. A., 2005, “Adiabatic Effectiveness Measurements of Endwall Film-Cooling for a First Stage Vane,” ASME J. Turbomach., 127, pp. 297–305.
[CrossRef]Thrift, A. A., Thole, K. A., and Hada, S., 2012, “Effects of Orientation and Position of the Combustor-Turbine Interface on the Cooling of a Vane Endwall,” ASME J. Turbomach., 134, p. 061019.
[CrossRef]Gao, Z., Narzary, D., and Han, J.-C., 2009, “Turbine Blade Platform Film Cooling With Typical Stator-Purge Flow and Discrete-Hole Film Cooling,” ASME J. Turbomach., 131, p. 041004.
[CrossRef]Narzary, D., 2009, “Experimental Study of Gas Turbine Blade Film Cooling and Heat Transfer,” Ph.D. thesis, Texas A&M University, College Station, TX.
Papa, M., Srinivasan, V., and Goldstein, R. J., 2012, “Film Cooling Effect of Rotor-Stator Purge Flow on Endwall Heat/Mass Transfer,” ASME J. Turbomach., 134, p. 041014.
[CrossRef]Suryanarayanan, A., Mhetras, S., Schobeiri, M. T., and Han, J. C., 2009, “Film Cooling Effectiveness on a Rotating Blade Platform,” ASME J. Turbomach., 131, p. 011014.
[CrossRef]Suryanarayanan, A., Ozturk, B., Schobeiri, M. T., and Han, J. C., 2010, “Film-Cooling Effectiveness on a Rotating Turbine Platform Using Pressure Sensitive Paint Technique,” ASME J. Turbomach., 132, p. 041001.
[CrossRef]Pau, M., Paniagua, G., Delhaye, D., de la Loma, A., and GinibreP., 2010, “Aerothermal Impact of Stator-Rim Purge Flow and Rotor-Platform Film Cooling on a Transonic Turbine Stage,” ASME J. Turbomach., 132, p. 021006.
[CrossRef]Schuepbach, P., Abhari, R. S., Rose, M. G., and Gier, J., 2011, “Influence of Rim Seal Purge Flow on Performance of an Endwall-Profiled Axial Turbine,” ASME J. Turbomach., 133, p. 021011.
[CrossRef]Green, B. R., Mathison, R. M., and Dunn, M. G., 2012, “Time-Averaged and Time-Accurate Aerodynamic Effects of Rotor Purge Flow for a Modern, One and One-Half Stage High-Pressure Turbine—Part II: Analytical Flow Field Analysis,” ASME Paper No. GT2012-69939.
[CrossRef]Reid, K., Denton, J., Pullan, G., Curtis, E., and Longley, J., 2006, “The Effect of Stator-Rotor Hub Sealing Flow on the Mainstream Aerodynamics of a Turbine,” ASME Paper No. GT2006-90838.
[CrossRef]BindonJ. P., 1980, “Exit Plane and Suction Surface Flows in an Annular Turbine Cascade With a Skewed Inlet Boundary Layer,” Int. J. Heat Fluid Flow, 2, pp. 57–66.
[CrossRef]Boletis, E., Sieverding, C. H., and Van HoveW., 1983, “Effect of Skewed Inlet Endwall Boundary Layer on the 3D-Flowfield in an Annular Cascade,” Paper No. AGARD-CP-351.
Walsh, J. A., and Gregory-Smith, D. G., 1987, “The Effect of Inlet Skew on the Secondary Flows and Losses in a Turbine Cascade,” IMechE Paper No. C275/87.
Barigozzi, G., Franchini, G., and Perdichizzi, A., 2007, “Inlet Turbulence Intensity Effect on Endwall Film Cooling,” Proceedings of the 7th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, Athens, Greece, March 5–9, pp. 1105–1116.
Gregory-Smith, D. G., Graves, C. P., and Walsh, J. A., 1988, “Growth of Secondary Losses and Vorticity in an Axial Turbine Cascade,” ASME J Turbomach., 110, pp. 1–8.
[CrossRef]Barigozzi, G., Fontaneto, F., Franchini, G., Perdichizzi, A., Maritano, M., and Abram, R., 2012, “Influence of Coolant Flow Rate on Aero-Thermal Performance of a Rotor Blade Cascade With Endwall Film Cooling,” ASME J. Turbomach., 134, p. 051038.
[CrossRef]Camci, C., Kim, K., and Hippensteele, S. A., 1992, “A New Hue Capturing Technique for the Quantitative Interpretation of Liquid Crystal Images Used in Convective Heat Transfer Studies,” ASME J. Turbomach., 114, pp. 765–775.
[CrossRef]Kost, F. H., and Holmes, A. T., 1985, “Aerodynamic Effect of Coolant Ejection in the Rear Part of Transonic Rotor Blades,” Paper No. AGARD-CP-390.
Mee, D. J., 1992, “Techniques for Aerodynamic Loss Measurement of Transonic Turbine Cascade With Trailing-Edge Region Coolant Ejection,” ASME Paper No. 92-GT-157.