Zess, G., and Thole, K., 1999, “Computational Design and Experimental Evaluation of Using a Leading Edge Fillet on a Gas Turbine Vane,” ASME Paper No. 2001-GT-0404.
Lethander, A., Thole, K., Zess, G., and Wagner, J., 2003, “Optimizing the Vane-Endwall Junction to Reduce Adiabatic Wall Temperatures in a Turbine Vane Passage,” ASME Paper No. GT2003-38940.
Hermanson, K., and Thole, K., 2000, “Effect of Inlet Conditions on Endwall Secondary Flows,” J. Propul. Power, 16 (2), pp. 286–296.
Munk, M., and Prim, R. C., 1947, “On the Multiplicity of Steady Gas Flows Having the Same Streamline Pattern,” Proc. Natl. Acad. Sci. U.S.A.
[CrossRef], 33 , pp. 137–141.
Lakshminarayana, B., 1975, “Effects of Inlet Temperature Gradients on Turbomachinery Performance,” ASME J. Eng. Power, 97 , pp. 64–74.
Langston, L. S., 1980, “Crossflows in a Turbine Cascade Passage,” ASME J. Eng. Power, 102 , pp. 866–874.
Colban, W. F., Thole, K. A., and Zess, G., 2002, “Combustor-Turbine Interface Studies-Part 1: Endwall Effectiveness Measurements,” ASME Paper No. GT2002-30526.
Colban, W. F., Thole, K. A., and Zess, G., 2002, “Combustor-Turbine Interface Studies-Part 2: Flow and Thermal Field Measurements,” ASME Paper No. GT2002-30527.
Kost, F., and Nicklas, M., 2001, “Film-Cooled Turbine Endwall in a Transonic Flow Field: Part I-Aerodynamic Measurements,” ASME Paper No. 2001-GT-0145.
Kang, M., Kohli, A., and Thole, K. A., 1999, “Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall,” ASME J. Turbomach.
[CrossRef], 121 (3), pp. 558–568.
Radomsky, R., and Thole, K. A., 2000, “High Freestream Turbulence Effects in the Endwall Leading Edge Region,” ASME J. Turbomach.
[CrossRef], 122 , pp. 699–708.
Blair, M. F., 1974, “An Experimental Study of Heat Transfer and Film Cooling on Large-Scale Turbine Endwalls,” ASME J. Heat Transfer, 96 (4), pp. 524–529.
Haldeman, C., and Dunn, M., 2004, “Heat-Transfer Measurements and Predictions for the Vane and Blade of a Rotating High-Pressure Turbine Stage,” ASME J. Turbomach.
[CrossRef], 126 , pp. 101–109.
Povey, T., Chana, K., Jones, T., and Hurrion, J., 2005, “The Effect of Hot-Streaks on HP Vane Surface and Endwall Heat Transfer: An Experimental and Numerical Study,” ASME Paper No. GT2005-69066.
Nicklas, M., 2001, “Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II-Heat Transfer and Film-Cooling Effectiveness Measurements,” ASME Paper No. 2001-GT-0146.
Graziani, R., Blair, M., Taylor, J., and Mayle, R., 1980, “An Experimental Study of Endwall and Airfoil Surface Heat Transfer in a Large Scale Turbine Blade Cascade,” ASME J. Eng. Power, 102 , pp. 257–267.
Haldeman, C. W., Dunn, M. G., MacArthur, C. D., and Murawski, C. G., 1992, “The USAF Advanced Turbine Aerothermal Research Rig (ATARR),” "NATO AGARD Propulsion and Energetics Panel Conference Proceedings", Vol. 527 , Antalya, Turkey.
Barringer, M. D., Thole, K. A., and Polanka, M. D., 2007, “Experimental Evaluation of an Inlet Profile Generator for High-Pressure Turbine Tests,” ASME J. Turbomach.
[CrossRef], 129 (2), pp. 382–393.
Jones, T. V., 1995, “The Thin Film Heat Transfer Gauge-A History and New Developments.” Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci., 209 (C510), pp. 150–160.
Moffat, R. J., 1982, “Contributions to the Theory of a Single-Sample Uncertainty Analysis,” ASME J. Fluids Eng., 104 , pp. 250–260.
Kang, M., and Thole, K. A., 2000, “Flowfield Measurements in the Endwall Region of a Stator Vane,” ASME J. Turbomach.
[CrossRef], 122 , pp. 458–466.
Barringer, M. D., Thole, K. A., and Polanka, M. D., 2009, “Effects of Combustor Exit Profiles on Vane Aerodynamic Loading and Heat Transfer in a High Pressure Turbine,” ASME J. Turbomach., 131 (2), p. 021008.