Hermanson, K., and Thole, K. A., 2000, “Effect of Mach Number on Secondary Flow Characteristics,” International Journal of Turbo and Jet Engines, vol. 17, pp. 179-196.
Hermanson, K., and Thole, K.A., 2000, “Effect of Inlet Profiles on Endwall Secondary Flows,” Journal of Propulsion and Power, vol. 16, no. 2, pp 286-296.
Radomsky, R., and Thole, K. A., 2000, “High Freestream Turbulence Effects in the Endwall Leading Edge Region,” Journal of Turbomachinery, vol. 122, pp. 699-708.
Zess, G. A. and Thole, K. A., 2002, “Computational Design and Experimental Evaluation of Using a Leading Edge Fillet on a Gas Turbine Vane,” Journal of Turbomachinery, vol. 124, no. 2, pp. 167-175.
Hermanson, K. and Thole, K. A., 2002, “Effect on Non-Uniform Inlet Conditions on Endwall Secondary Flows,” Journal of Turbomachinery, vol. 124, pp. 623-631.
Lethander, A. and Thole, K. A., 2004, “Optimizing the Vane-Endwall Junction to Reduce Adiabatic Wall Temperatures in a Turbine Vane Passage,” AIAA Journal of Propulsion and Power, vol. 20, pp. 1105-1116.
Knost, D. and Thole, K. A., 2005, “Computational Predictions of Endwall Film-Cooling for a First Stage Vane,” International Journal of Turbo and Jet Engines, vol. 22, pp. 41-58.
Knost, D. G., and Thole, K. A.,2005, “Adiabatic Effectiveness Measurements of Endwall Film-Cooling for a First Stage Vane,” Journal of Turbomachinery, vol. 127, pp. 297-305.
Ranson, W., Thole, K. A., and Cunha, F., 2005, “Adiabatic Effectiveness Measurements and Predictions of Leakage Flows Along a Blade Endwall,” Journal of Turbomachinery, vol. 127, pp. 609-618.
Thole, K. A. and Knost, D., 2005, “Heat Transfer and Film-Cooling for the Endwall of a First Stage Turbine Vane,” International Journal of Heat and Mass Transfer, vol. 48, issues 25-26, pp. 5255-5269.
Cardwell, N., Sundaram, N., and Thole, K. A., 2006, “Effects of Roughness and Mid-Passage Gap on Endwall Film Cooling,” Journal of Turbomachinery, vol. 128, pp. 62-70.
Colban, W. and Thole, K. A., 2007, “Influence of Hole Shape on the Performance of a Turbine Vane Endwall Film-Cooling Scheme,” International Journal of Heat and Fluid Flow, vol. 28, Issue 3, pp. 341-356.
Colban, W. F., Lethander, A. T., Thole, K. A., and Zess, G., 2002, “Combustor-Turbine Interface Studies: Part 2: Flow and Thermal Field Measurements,” Journal of Turbomachinery, vol. 125, pp.203-209.
Colban, W. F., Thole, K. A., and Zess, G., 2002, “Combustor-Turbine Interface Studies: Part 1: Endwall Measurements,” Journal of Turbomachinery, vol. 125, pp.193-202.
Sundaram, N. and Thole, K. A., 2007, “Effects of Surface Deposition, Hole Blockage, and TBC Spallation on Vane Endwall Film-Cooling,” Journal of Turbomachinery, vol. 129, pp. 599-607.
Cardwell, N., Sundaram, N., and Thole, K. A., 2007, “The Effects of Varying the Combustor-Turbine Gap,” Journal of Turbomachinery, vol. 129, pp. 756-764. (Best Paper Award for Gas Turbine Heat Transfer)
Colban, W., Thole, K. A., and Haendler, M., 2008, “A Comparison of Cylindrical and Fan-Shaped Film-Cooling Holes on a Vane Endwall at Low and High Freestream Turbulence Levels,” Journal of Turbomachinery, vol. 130, pp. 031007.
Lynch, S. P. and Thole, K. A., 2008, “The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane,” Journal of Turbomachinery. vol. 130, pp. 041019.
Sundaram, N. and Thole, K. A., 2008, “Bump and Trench Modifications to Film-Cooling Holes at the Vane Endwall Junction,” Journal of Turbomachinery. vol. 130, pp. 041013.
Sundaram, N. and Thole, K. A., 2009, “Film-Cooling Flowfields with Trenched Holes on an Endwall,” Journal of Turbomachinery, vol. 131, pp. 041007.
Hada, S. and Thole, K. A., 2011, “Computational Study of a Midpassage Gap and Upstream Slot on Vane Endwall Film-Cooling,” Journal of Turbomachinery, vol. 133, pp. 011024.
Lynch, S. P., Sundaram, N., Thole, K. A., Kohli, A., Lehane, C., 2011, “Heat Transfer for a Turbine Blade with Non-Axisymmetric Endwall Contouring,” Journal of Turbomachinery, vol. 133, 011019.
Lynch, S. and Thole, K. A., 2011, “The Effect of the Combustor-Turbine Slot and Mid-Passage Gap on Vane Endwall Heat Transfer,” Journal of Turbomachinery, vol. 133, pp. 041002.
Lynch, S. P., Thole, K. A., Kohli, A., Lehane, C., 2011, “Computational Predictions of Heat Transfer and Film-Cooling for a Turbine Blade with Non-Axiymmetric Endwall Contouring,” Journal of Turbomachinery, vol. 133, pp. 041003.
Thrift, A. A., Thole, K. A., Hada, S., 2011, “Effects of an Axisymmetric Contoured Endwall on a Nozzle Guide Vane: Adiabatic Effectiveness Measurements,” Journal of Turbomachinery, vol. 133, pp. 041007.
Thrift, A. A., Thole, K. A., Hada, S., 2011, “Effects of an Axisymmetric Contoured Endwall on a Nozzle Guide Vane: Heat Transfer Measurements,” Journal of Turbomachinery, vol. 133, pp. 041008.
Thrift, A. A. and Thole, K. A., 2012, “Influence of Flow Injection Angle on a Leading-Edge Horseshoe Vortex,” International Journal of Heat and Mass Transfer, vol. 55, pp 4651-4664.
Thrift, A. A., Thole, K. A., Hada, S., 2012,“Effects of Orientation and Position of the Combustor-Turbine Interface Gap on the Cooling of a Vane Endwall,” Journal of Turbomachinery, vol. 123, pp 061019.
Thrift, A. A., Thole, K. A., Hada, S., 2013, “Impact of the Combustor-Turbine Interface Slot Orientation on the Durability of a Nozzle Guide Vane Endwall,” Journal of Turbomachinery, vol. 135, pp. 041019.
Mensch, A. and Thole, K. A., Craven, B., 2014, Conjugate Heat Transfer Measurements and Predictions of a Blade Endwall with a Thermal Barrier Coating,” Journal of Turbomachinery, vol. 136, pp. 121003.
Mensch, A. and Thole, K. A., 2014, “Overall Effectiveness of a Blade Endwall with Jet Impingement and Film Cooling,” Journal of Engineering for Gas Turbines and Power, vol. 136, pp. 031901.
Mensch, A. and Thole, K., 2015, “Simulations of Multiphase Particle Deposition on a Gas Turbine Endwall with Impingement and Film Cooling,” Journal of Turbomachinery, vol. 137, pp 111002.
Mensch, A. E. and Thole, K. A., 2015, “Conjugate Heat Transfer Analysis of the Effects of Impingement Channel Height for a Turbine Blade Endwall,” International Journal of Heat and Mass Transfer, vol. 82C, pp. 66-77.
Mensch, A., Thole, K. A., 2016, “Effects of Non-axisymmetric Endwall Contouring and Film Cooling on the Passage Flowfield in a Linear Turbine Cascade,” Experiments in Fluids, DOI 10.1007/s00348-015-2093-5, vol 57:1.
Mensch, A. and Thole, K. A., 2015, “Overall Effectiveness and Flowfield Measurements for an Endwall with Non-Axisymmetric Contouring,” Journal of Turbomachinery, vol. 138, pp 031007.
Lynch, S., Thole, K. A., 2016, “Comparison of the Three-Dimensional Boundary Layer on Flat Versus Contoured Endwall, “Journal of Turbomachinery, vol. 138, pp 041008.
Lynch, S., Thole, K. A., 2017, “Heat Transfer and Film Cooling on a Contoured Blade Endwall with Platform Gap Leakage,” Journal of Turbomachinery, vol. 139(5), pp. 051002.
DeShong, E., Siroka, S., Berdanier, R., Thole, K. A., 2022, “Evaluating the Influence of Rotor-Casing Eccentricity on Turbine Efficiency Including Time-Resolved Flow Field Measurements,” J of Turbomachinery, vol. 144 (2), pp. 021012.