Commercial Aircraft Propulsion and Energy Systems Research: Reducing the Global Carbon Emissions, National Academies of Sciences, Engineering, Medicine, committee member [Visit Site]
Advanced Technologies for Gas Turbines, National Academies of Sciences, Engineering, Medicine, committee co-chair [Visit Site]
4. Thole, K. A., 2022, “From Watching Planes in the Sky to Making Turbines More Efficient,” Women in Mechanical Engineering – Energy & Environment (Springer).
3. Bogard, D. G. and Thole, K. A., 2007, “Gas Turbine Film Cooling,” Turbine Science and Technology (AIAA Progress in Astronautics and Aeronautics: AIAA).
2. Bogard, D. G., and Thole, K. A., 1998, “Wall Bounded Turbulent Flows,” CRC Handbook of Fluid Dynamics (Boca Raton: Chemical Rubber Company, CRC Press) Section 13.5, pp. 13.49 – 13.63.
1. Bogard, D. G., and Thole, K. A., 1998, “Coherent Structures,” CRC Handbook of Fluid Dynamics (Boca Raton: Chemical Rubber Company, CRC Press) Section 13.4, pp. 13.40 – 13.48.
147. Wilkins, P. H., Lynch, S. Pl, Thole, K. A., Vincent, T., Quach, S., Mongillo, D., 2022, “Effect of Ceramic Matrix Composite Surface on Film Cooling,” Journal of Turbomachinery,., vol. 144(8), pp. 081014.
146. Siroka, S., Berdanier, R. A., Thole, K. A., 2022, “Development of Coated Heat Flux Gauges for Fast Responding Measurements,” Measurement Science and Technology, vol. 33, pp. 045104.
145. Siroka, S., Berdanier, R. A., Thole, K. A., 2022, “Two-Layer Transient Heat Transfer Using Impulse Response Methods,” International Journal of Heat and Mass Transfer, vol. 187 (15), pp. 122511.
144. DeShong, E, Peters, B., Berdanier, R., Thole, K., Paynabar, K. and Gabraeel, N., 2022, “Correlating Time-Resolved Pressure Measurements with Rim Sealing Effectiveness for Real-Time Turbine Health Monitoring”, J of Turbomachinery, vol. 144 (6), pp. 061004.
143. Cory, T., Edelson, R., and Thole, K. A., Tyler, V., Quach, S. and Mongillo, D., 2022, “Impact of Ceramic Matrix Composite Topology on Friction Factor and Heat Transfer,” J of Turbomachinery, vol 144 (3), pp. 031003.
142. 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.
141. Stafford, G., McClain, S., Hanson, D.R., Kunz, R. F., Thole, K. A., 2022, “Convection in Scaled Turbine Internal Cooling Passages with Additive Manufacturing Roughness,” J of Turbomachinery, vol. 144(4), pp. 041008.
140. Thole, K. A., Lynch, S. P., Wildgoose, A., 2021, “Review of Advances in Convective Heat Transfer Developed through Additive Manufacturing” Adv in Heat Transfer, vol. 53, pp. 249-325.
139. Siroka, S., Foley, B., Berdanier, R. A., Thole, K. A., 2021, “Application of 3-omega method for thin-film heat flux gauge calibration,” Measurement Science and Technology, vol. 32, No. 11, pp. 114001.
138. Leung, S. L., Hargrove, B., Marsh, E., Gregg, A., & Thole, K. (2020). Prompting by COVID-19 to Rethink the Purpose of Engineering Laboratory Education – Develop Practical Competence to Solve Real-World Problem. Advances in Engineering Education, 8(4).
137. McClain, S. T., Hanson, D. R., Cinnamon, E., Snyder, J. C., Kunz, R. F., Thole, K. A., “Flow in a Simulated Turbine Blade Cooling Channel with Spatially Varying Roughness Caused by Additive Manufacturing Orientation,” Journal of Turbomachinery, vol. 143(7), pp. 071013 https://doi.org/10.1115/1.4050389
136. Wildgoose, A. J., Thole, K. A., Sanders, P. Wang, L., 2021, “Impact of Additive Manufacturing on Internal Cooling Channels with Varying Diameters and Build Directions,” Journal of Turbomachinery, vol. 143 (7), pp. 071003 https://doi.org/10.1115/1.4050336.
135. Huelsmann, N. C., Thole, K. A., 2021, “Effects of Jet Impingement on Convective Heat Transfer in Effusion Holes,” Journal of Turbomachinery, vol. 143 (6), pp. 061011 https://doi.org/10.1115/1.4050335.
134. Wilkins, P. H., Lynch, S. P., Thole, K. A., Quach, S., Vincent, T., 2021, “Experimental Heat Transfer and Boundary Layer Measurements on a Ceramic Matric Composite Surface,” Journal of Turbomachinery, vol. 143 (6), pp. 061010 https://doi.org/10.1115/1.4050314.
133. Knisely, B. F., Berdanier, R. A., Thole, K. A., Haldeman, C. W., Markham, J. R., Cosgrove, J. E., Carlson, A. E., Scire, J. J., 2021, “Acquisition and Processing Considerations for Infrared Images of Rotating Turbine Blades,” Journal of Turbomachinery, vol. 143 (4), pp. 041013. https://doi.org/10.1115/1.4050143
132. Berdanier, R. A., DeShong, E. T., Thole, K. A., Robak, 2021 “Evaluating the Effects of Transient Purge Flow on Stator-Rotor Seal Performance,” Journal of Turbomachinery, vol. 143 (2), pp. 021006.
131. Siroka, S., Berdanier, R. A., Thole, K. A., Chana, K., Haldeman, C. W., and Anthony, R. J., 2020 “Comparison of Thin Film Heat Flux Gauge Technologies Emphasizing Continuous-Duration Operation,” Journal of Turbomachinery, vol. 142(9), pp. 091001.
130. Snyder, J. C. and Thole, K. A., 2020, “Tailoring Surface Roughness Using Additive Manufacturing to Improve Internal Cooling,” Journal of Turbomachinery, vol. 142(7), pp. 071004.
129. Monge-Concepción, I, Berdanier, R. A., Barringer, M. B., Thole, K. A. and Robak, C., 2020, “Evaluating the Effect of Vane Trailing Edge Flow on Turbine Rim Sealing” Journal of Turbomachinery, vol. 142(8), pp. 081001.
128. Snyder, J. C. and Thole, K. A., 2020, “Performance of Public Film Cooling Geometries Produced through Additive Manufacturing” Journal of Turbomachinery, vol. 142(5), pp. 051009.
127. Snyder, J. C. and Thole, K. A., 2020, “Effect of Additive Manufacturing Process Parameters on Turbine Cooling” Journal of Turbomachinery, vol. 142(5), pp051007.
126. Berdanier, R. A., Monge-Concepcion, I., Knisely, B. F., Barringer, M., Thole, K. A., Grover, E., 2019, “Scaling Sealing Effectiveness in a Stator-Rotor Cavity for Differing Blade Spans,” Journal of Turbomachinery, Vol. 141 (5), pp. 051007.
125. Kirsch, K. and Thole, 2018, “Numerical Optimization, Characterization, and Experimental Investigation of Additively Manufactured Communicating Microchannels” Journal of Turbomachinery, Vol. 140 (11), pp. 111003.
124. Stimpson, C., Snyder, J., Thole, K. A., and Mongillo, D., 2018 “Effects of Coolant Feed Direction on Additively Manufactured Film Cooling Holes” Journal of Turbomachinery, Vol 140(11), pp. 111001.
123. Kirsch, K. L. and Thole, K. A., 2018, “Isolating the Effects of Surface Roughness versus Wall Shape in Numerically Optimized, Additively Manufactured Micro Cooling Channels,” Experimental Thermal and Fluid Science, Vol. 98, p. 227-238.
122 Shrager, A., Thole, K. A., and Mongillo, D., 2018 “Effects of Effusion Cooling Pattern Near the Dilution Hole for a Double-Walled Combustor Liner – Part 1: Overall Effectiveness Measurements”, Journal of Engineering for Gas Turbines and Power, Vol. 141 (1), pp. 011022.
121 Shrager, A., Thole, K. A., and Mongillo, D., 2018 “Effects of Effusion Cooling Pattern Near the Dilution Hole for a Double-Walled Combustor Liner – Part 2: Flowfield Measurements”, Journal of Engineering for Gas Turbines and Power, Vol. 141 (1), pp. 011023.
120 Clark, K., Barringer, M., Johnson, D., Thole, K. A., Grover, E., and Robak, C., 2018 “Effects of Purge Flow Configuration on Sealing Effectiveness in a Rotor-Stator Cavity” Journal of Engineering for Gas Turbines and Power, vol. 140(11), pp. 112502.
119 Town, J., Straub, D. Black, J., Thole, K. A., and Shih, T., 2018 “State-of-the-Art Cooling Technology for a Turbine Rotor Blade,” Journal of Turbomachinery, vol. 140 (7), pp. 071007.
118 Stimpson, C. K., Snyder, J. C., Thole, K. A., and Mongillo, D., 2017 “Effectiveness Measurements of Additively Manufactured Film Cooling Holes” Journal of Turbomachinery, vol. 140(1), pp. 011009.
117 Kirsch, K., and Thole, K. A., 2017 “Experimental Investigation of Numerically Optimized Wavy Microchannels Created Through Additive Manufacturing” Journal of Turbomachinery, vol. 140(2), pp. 021002.
116 Ferster, K., Kirsch, K., and Thole, K. A., 2017 “Effects of Geometry and Spacing in Additively Manufactured Microchannel Pin Fin Arrays” Journal of Turbomachinery, vol. 140(1), pp. 011007.
115 Kirsch, K. and Thole, K. A., 2017, “Pressure Loss and Heat Transfer Performance for Additively and Conventionally Manufactured Pin Fin Arrays,” International Journal of Heat and Mass Transfer, vol. 108, pp. 2502-2513.
114 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.
113 Clark, K., Barringer, M., Thole, K., Clum, C., Hiester, P., Memory, C., Robak, C., 2016, “Effects of Purge Distribution and Flowrates on Vane Rim Sealing,” Journal of Engineering for Gas Turbines and Power, vol. 139(3), pp. 031904.
112 Schroeder, R., Thole, K. A., 2016, “Thermal Field Measurements for a Shaped Hole at Low and High Freestream Turbulence Intensity,” Journal of Turbomachinery, vol. 139(2), pp. 021012.
111 Schroeder, R., Thole, K. A., 2016, “Effect of In-Hole Roughness on Film Cooling from a Shaped Hole,” Journal of Turbomachinery, vol. 139(3), pp. 031004.
110 Kirsch, K. and Thole, K. A., 2016, “Heat transfer and Pressure Loss Measurements in Additively Manufactured Wavy Microchannels,” Journal of Turbomachinery, vol 139(1), pp. 011007 (2016 Best Paper Award for Gas Turbine Heat Transfer).
109 Stimpson, C., Snyder, J., Thole, K. A., and Mongillo, D., 2016, “Scaling Roughness Effects on Pressure Loss and Heat Transfer of Additively Manufactured Channels,” Journal of Turbomachinery, vol. 139(2), pp. 021003.
108 Schroeder, R. P., and Thole, K. A., 2016, “Effect of High Freestream Turbulence on Flowfields of Shaped Film Cooling Holes,” Journal of Turbomachinery, vol. 138, pp 091001.
107 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.
106 Snyder, J., Stimpson, C., Thole, K. A., and Mongillo, D., 2016, “Build Direction Effects on Additively Manufactured Channels,” Journal of Turbomachinery, vol. 138, pp 051006.
105 Stimpson, C., Snyder, J., Thole, K. A., and Mongillo, D., 2016, “Roughness Effects on Flow and Heat Transfer for Additively Manufactured Channels,” Journal of Turbomachinery, vol. 138, pp. 051008.
104 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.
103 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.
102 Snyder, J. C., Stimpson, C. K., Thole, K. A., Mongillo, D. J., 2015, “Build Direction Effects on Micro-Channel Tolerance and Surface Roughness,” Journal of Mechanical Design, vol. 137, pp. 111714.
101 Whitfield, C. A., Schroeder, R. P., Thole, K. A., Lewis, S. D., 2015, “Blockage Effects from Simulated Thermal Barrier Coatings for Cylindrical and Shaped Holes,” Journal of Turbomachinery, vol. 137, pp 091004.
100 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.
99 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.
98 Kirsch, K. L. and Thole, K. A., 2015 “Heat Transfer Measurements of Oblong Pins,” Journal of Turbomachinery, vol. 137, pp 071004.
97 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.
96 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.
95 Eberly, M. K. and Thole, K. A., 2013, “Time-Resolved Film-Cooling Flows at High and Low Density Ratios,” Journal of Turbomachinery, vol. 136, pp. 061003 (Best Paper Award for Gas Turbine Heat Transfer).
94 Kirsch, K.L., Ostanek, J. K., and Thole, K. A., 2013, “Comparison of Pin Surface Heat Transfer in Arrays of Oblong and Cylindrical Pin Fins,” Journal of Turbomachinery, vol. 136, pp 041015.
93 Barringer, M., Thole, K. A., Krishnan, V., Landrum, E., 2013, “Manufacturing Influences on Pressure Losses of Channel Fed Holes,” Journal of Turbomachinery, vol. 136, pp. 051012.
92 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.
91 Lawson, S., Lynch, S., and Thole, K. A., 2013, “Simulations of Multi-Phase Particle Deposition on a Non-Axisymmetric Contoured Endwall with Film-Cooling,” Journal of Turbomachinery, vol. 135, pp. 031032.
90 Barringer, M.D., Thole, K. A., Breneman, D. L., Tham, K-M, and Laurello, V., 2013, “Effects of Centrifugal Forces on Particle Deposition for a Representative Seal Pin Between Two Blades,” Journal of Engineering for Gas
Turbines and Power, vol. 135, pp. 032601.
89 Musgrove, G. O., Thole, K. A., Grover, E., and Barker, J., 2012, “Performance Measurements of a Unique Louver Particle Separator for Gas Turbine Engines,” Journal of Engineering for Gas Turbines and Power, vol. 135, pp. 012001.
88 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.
87 Ostanek, J., Thole, K. A., 2012, “Effect of Streamwise Spacing on Periodic and Random Unsteadiness in a Bundle of Short Cylinders Confined in a Channel,” Experiments in Fluids, vol. 53, pp. 1779-1796.
86 Lawson, S. and Thole, K. A., 2012, “Simulations of Multi-Phase Particle Deposition on Endwall Film-Cooling Holes in Transverse Trenches, 2012,” Journal of Turbomachinery, vol. 134, pp. 051040.
85 Lawson, S., Thole, K. A., Okita, Y. and Nakamata, C., 2012, “Simulations of Multi-Phase Particle Deposition on a Showerhead with Staggered Film-Cooling Holes,” Journal of Turbomachinery, vol. 134, pp. 051041.
84 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.
83 Ostanek, J. K. and Thole, K. A., 2012, “Wake Development in Staggered Short Cylinder Arrays within a Channel,” Experiments in Fluids, vol. 53, pp. 673–697.
82 Ostanek, J. and Thole, K. A., 2012, “Flowfield Measurements in a Single Row of Low Aspect Ratio Pin-Fins,” Journal of Turbomachinery, vol. 134, pp 051034.
81 Lawson, S. A. and Thole, K. A., 2012, “Simulations of Multi-Phase Particle Deposition on Endwall Film-Cooling,” Journal of Turbomachinery, vol. 134, pp. 011003.
80 Cardwell, N. D., Vlachos, P. P., and Thole, K. A., 2011, “A Multi-Parametric Particle Pairing Algorithm for Particle Tracking in Single and Multiphase Flows,” Measurement Science and Technology, vol. 22, 105406.
79 Lawson, S. A., Thrift, A. A., Thole, K. A., Kohli, A., 2011 “Heat Transfer from Multiple Row Arrays of Low Aspect Ratio Pin Fins,” International Journal of Heat and Mass Transfer, vol. 54, pp. 4099-4109.
78 Weaver, S., Barringer, M., Thole, K. A., 2011, “Micro Channels with Manufacturing Roughness Levels,” Journal of Turbomachinery, vol. 134, pp. 041014.
77 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.
76 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.
75 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.
74 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.
73 Cardwell, N. D., Vlachos, P. P., Thole, K. A., 2011, “A Method for Identifying and Visualizing Foreign Particle Motion Using Time Resolved Particle Tracking Velocimetry,” Journal of Turbomachinery, vol. 133, pp. 021021.
72 Lawson, S. A. and Thole, K. A., 2011, “Effects of Simulated Particle Deposition on Film Cooling,” Journal of Turbomachinery, vol. 133, pp. 021009 (Best Paper Award for Gas Turbine Heat Transfer).
71 Carullo, J., Nasir, S., Ng, W., Thole, K., Wu, H., Moon, H. K., 2011 “The Effects of Large Scale High Freestream Turbulence, and Exit Reynolds Number on Turbine Vane Heat Transfer in a Transonic Cascade,” Journal of Turbomachinery, vol. 131, pp. 011030.
70 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.
69 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.
68 Colban, W., Thole, K. A., Bogard, D., 2011, “A Film Cooling Correlation for Shaped Holes on a Flat-Plate Surface,” Journal of Turbomachinery, vol. 133, pp. 011002.
67 Lyall, M. E., Thrift, A. A., Thole, K. A., and Kohli, A., 2011, “Heat Transfer from Low Aspect Ratio Pin Fins,” Journal of Turbomachinery, vol. 133, pp. 011001.
66 Cardwell, N. D., Vlachos, P. P., Thole, K. A., 2011, “Developing and Fully Developed Turbulent Flow in Ribbed Channels,” Experiments in Fluids, vol. 50, pp. 1357-1371.
65 Thrift, A. A., Brumbaugh, S., Thole, K. A., Kohli, A., 2010, “A Methodology to Measure Aerodynamic Forces on Cylinders in Channel Flow,” Journal of Fluids Engineering, vol. 132, pp. 081401.
64 Ostanek, J., Thole, K. A., Prausa, J., and Van Suetendael, A., 2010, “Establishing a Methodology for Resolving Convective Heat Transfer from Complex Geometries,” Journal of Turbomachinery, vol. 132, pp. 031014.
63 Land, C., Thole, K. A., Joe, C., 2010, “Considerations of a Double-Wall Cooling Design to Reduce Sand Blockage,” Journal of Turbomachinery, vol. 132, pp. 031011.
62 Cardwell, N. D., Burd, S. W., Thole, K. A., 2010, “Investigation of Sand Blocking within Impingement and Film-Cooling Holes,” Journal of Turbomachinery, vol. 132, pp. 021020.
61 Nasir, S., Carullo, J., Ng, W., Thole, K. A., Wu, H. Zhang, L., Moon, H., 2009, “Effects of Large Schale High Freestream Turbulence and Exit Reynolds Number on Turbine Vane Heat Transfer in a Transonic Rig,” Journal of Turbomachinery, vol. 131, pp. 021021.
60 Sundaram, N. and Thole, K. A., 2009, “Film-Cooling Flowfields with Trenched Holes on an Endwall,” Journal of Turbomachinery, vol. 131, pp. 041007.
59 Barringer, M., Thole, K. A., and Polanka, M. D., 2009, “Effects of Combustor Exit Profiles on High Pressure Turbine Vane Aerodynamics and Heat Transfer,” Journal of Turbomachinery, vol. 131, pp. 021008.
58 Barringer, M. D., Thole, K. A., and Polanka, M.D., 2009, “An Experimental Study of Combustor Exit Profile Shapes on Endwall Heat Transfer in High Pressure Turbine Vanes,” Journal of Turbomachinery, vol. 131, pp. 021009.
57 Barringer, M.D., Thole, K. A., Polanka, M. D., Clark, J. P., and Koch, P. J., 2009, “Migration of Combustor Exit Profiles Through High Pressure Turbine Vanes,” Journal of Turbomachinery, vol. 131, pp. 021010.
56 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.
55 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.
54 Sundaram, N., Barringer, M. D., and Thole, K. A., 2008, “Effects of Deposits on Film Cooling of a Vane Endwall Along the Pressure Side,” Journal of Turbomachinery, vol. 130, pp. 0410006.
53 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.
52 Lawson, M. and Thole, K. A., 2008, “Heat Transfer Augmentation along the Tube Wall of a Louvered Fin Heat Exchanger Using Practical Delta Winglets,” International Journal of Heat and Mass Transfer, vol. 51, pp. 2346-2360.
51 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)
50 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.
49 Scrittore, J., Thole, K. A., and Burd, S., 2007, “Investigation of Velocity Profiles for Effusion Cooling of Combustor Liners,” Journal of Turbomachinery, vol. 129, pp. 518-526.
48 Colban, W., Thole, K. A., and Haendler, M., 2007, “Experimental and Computational Comparisons of Fan-Shaped Film-Cooling on a Turbine Vane Surface,” Journal of Turbomachinery, vol. 129, pp. 23-31.
47 Barringer, M. D., Thole, K. A., and Polanka, M. D., 2007, “Experimental Evaluation of an Inlet Profile Generator for High-Pressure Turbine Tests,” Journal of Turbomachinery, vol. 129, pp. 382-393.
46 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.
45 Sanders, P. and Thole, K. A., 2006, “Effects of Winglets to Augment Tube Wall Heat Transfer in Louvered Fin Heat Exchangers,” International Journal of Heat and Mass Transfer, vol. 49, Issue 21-22, pp. 4058-4069.
44 Sewall, E. A., Tafti, D. K., Graham, A., Thole, K. A., 2006, “Experimental Validation of Large Eddy Simulations of Flow and Heat Transfer in a Stationary Ribbed Duct,” International Journal of Heat and Fluid Flow, vol. 27, Issue 2, pp. 243-258. (top 10 cited paper from 2005-2010 in the International Journal of Heat and Fluid Flow)
43 Bogard, D. G. and Thole, K. A., 2006, “Gas Turbine Film Cooling,” AIAA Journal of Propulsion (invited review paper), vol. 22, pp. 249-271.
42 Colban, W., Gratton, A., Thole, K. A., and Haendler, M., 2006, “Heat Transfer and Film-Cooling Measurements on a Stator Vane with Fan-Shaped Cooling Holes,” Journal of Turbomachinery, vol. 128, pp. 53-61.
41 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.
40 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.
39 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.
38 Pang, Y., Scott, E. P., Chen, J. Z., and Thole, K. A., 2005, “Electrical and Thermal Layout Design and Optimization Considerations for DPS Active IPEM,” Journal of Electronic Packaging, vol. 127, pp. 59-66.
37 Christophel, J. R., Thole, K., and Cunha, F, 2005, “Cooling the Tip of a Turbine Blade Using Pressure Side Holes—Part 2: Heat Transfer Measurements,” Journal of Turbomachinery, vol. 127, pp. 278-286.
36 Christophel, J. R., Thole, K., and Cunha, F, 2005, “Cooling the Tip of a Turbine Blade Using Pressure Side Holes—Part 1: Film Effectiveness Measurements,” Journal of Turbomachinery, vol. 127, pp. 270-277.
35 Christophel, J. R., Couch, E., Thole, K., and Cunha, F., 2005, “Measured Adiabatic Effectiveness and Heat Transfer for Blowing from the Tip of a Turbine Blade,” Journal of Turbomachinery, vol. 127, pp. 251-262.
34 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.
33 Couch, E., Christophel, J. R., Hohlfeld, E., Thole, K. and Cunha, F., 2005, “Comparison of Measurements and Predictions for Blowing from the Tip of a Turbine Blade,” AIAA Journal of Propulsion and Power, vol. 21, no. 2, pp. 335-343.
32 Stephan, R. and Thole, K. A., 2005, “Optimization Study Relevant to Louvered Fin Compact Heat Exchangers,” International Journal of Compact Heat Exchangers, Vol. VI, no. 1, 73-92.
31 Hohlfeld, E., Couch, E., Christophel, J. and Thole, K. A., 2005, “Predictions of Cooling from Dirt Purge Holes Along the Tip of a Turbine Blade,” International Journal of Turbo and Jet Engines, vol. 22, pp. 139-152.
30 Vakil, S. and Thole, K. A., 2005, “Flow and Thermal Field Measurements in a Combustor Simulator Relevant to a Gas Turbine Aero-Engine,” Journal of Engineering for Gas Turbines and Power, vol. 127, pp. 257-26730.
29 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.
28 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.
27 Ebeling, C., and Thole, K. A., 2004, “Measurements and Predictions of the Heat Transfer at the Tube-Fin Junction for Louvered Fin Heat Exchangers,” International Journal of Compact Heat Exchangers, vol. V, pp. 265-286.
26 Stitzel, S. and Thole, K. A., 2004, “Flow Field Computations of Combustor-Turbine Interactions Relevant to a Gas Turbine Engine,” Journal of Turbomachinery, vol. 126, pp.122-129.
25 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.
24 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.
23 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.
22 Barringer, M. D., Richard, O. T., Walter, J. P., Stitzel, S. M., and Thole, K. A., 2002, “Flow Field Simulations of a Gas Turbine Combustor,” Journal of Turbomachinery, vol. 124, pp. 508-516.
21 Lyman, A. C., Stephan, R. A., and Thole, K. A., Zhang, L., Memory, S., 2002 “Scaling of Heat Transfer Coefficients Along Louvered Fins,” Experimental Thermal Fluid Science, vol. 26, no. 5 pp 547-563.
20 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.
19 Thole, K. A., Radomsky, R., Kang, B., and Kohli, A., 2002, “Elevated Freestream Turbulence Effects on Heat Transfer for a Gas Turbine Vane,” International Journal of Heat and Fluid Flow, vol. 23, pp. 137-147.
18 Radomsky, R. and Thole, K. A., 2002, “Detailed Boundary Layer Measurements on a Turbine Stator Vane at Elevated Freestream Turbulence Levels,” Journal of Turbomachinery, vol. 124, pp. 107-118.
17 Harrington, M., McWaters, M., Bogard, D., Lemmon, C., and Thole, K. A., 2001, “Full-Coverage Film Cooling with Short Normal Injection Holes,” Journal of Turbomachinery, vol. 123, pp. 798-805.
16 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.
15 Radomsky, R., and Thole, K. A., 2000, “Measurements and Predictions of a Highly Turbulent Flowfield in a Turbine Vane Passage,” Journal of Fluids Engineering, vol. 122, pp. 666-676.
14 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.
13 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.
12 Kang, M., and Thole, K. A., 2000, “Flowfield Measurements in the Endwall Region of a Stator Vane,” Journal of Turbomachinery, vol. 122, pp. 458-466.
11 Radomsky, R., and Thole, K. A., 2000, “Flowfield Measurements for a Highly Turbulent Flow in a Stator Vane Passage,” Journal of Turbomachinery, vol. 122, no. 2, pp. 255-262.
10 Springer, M.E., and Thole, K. A., 1999, “Entry Region of Louvered Fin Heat Exchangers,” Experimental Thermal and Fluid Science, vol. 19, pp. 223-232.
9 Kang, M., Kohli, A., and Thole, K. A., 1999, “Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall,” Journal of Turbomachinery, vol. 121, pp. 558-568.
8 Springer, M., and Thole, K. A., 1998, “Experimental Design for Flowfield Studies of Louvered Fins,” Experimental Thermal and Fluid Science, vol. 18, no. 3, pp. 258-269.
7 Thole, K. A., Gritsch, M., Schulz, A., and Wittig, S., 1998, “Flowfield Measurements for Cooling Holes with Expanded Exits,” Journal of Turbomachinery, vol. 120, no. 2, pp. 327-336.
6 Thole, K. A., Gritsch, M., Schulz, A., Wittig, S., 1997, “Effects of a Crossflow at the Entrance to a Film-Cooling Hole,” Journal of Fluids Engineering, vol. 119, no. 3, pp. 533-540.
5 Thole, K. A., and Bogard, D. G., 1996, “High Freestream Turbulence Effects on Turbulent Boundary Layers,” Journal of Fluids Engineering, vol. 118, no. 2, pp. 276-284.
4 Laudon, M. F., Thole, K. A., Engelstad, R. L., Resnick, D. J., Cummings, K. D., and Dauksher, W. J., 1995, “Thermal Analysis of X-ray Membrane in a Plasma Environment,” Journal of Vacuum Science Technology B, vol. 13, no. 6, pp. 3050-3054.
3 Thole, K. A., and Bogard, D. G., 1995, “Enhanced Heat Transfer and Skin Friction due to High Freestream Turbulence,” Journal of Turbomachinery, vol. 117, no. 3, pp. 418-424.
2 Thole, K. A., and Bogard, D. G., 1994, “A Technique for Simultaneous Temperature and Velocity Measurements,” Measurement Science and Technology, vol. 5, pp. 435-439.
1 Thole, K. A., Bogard, D. G. and Whan-Tong, J., 1994, “Generating High Freestream Turbulence Levels,” Experiments in Fluids, vol. 17, pp. 375-380.
Peer Reviewed Conference Publications
149 Knisely, B. F., Berdanier, R. A., Thole, K. A., Haldeman, C. W., Markham, J. R., Cosgrove, J. E., Carlson, A. E., Scire, J. J., “Acquisition and Processing Considerations for Infrared Images of Rotating Turbine Blades,” International Gas Turbine and Aeroengine Congress and Exposition, GT2020-15522.148 Wildgoose, A. J., Thole, K. A., Sanders, P. Wang, L., “Impact of Additive Manufacturing on Internal Cooling Channels with Varying Diameters and Build Directions,” International Gas Turbine and Aeroengine Congress and Exposition, GT2020-15049.
147 Huelsmann, N. C., Thole, K. A., “Effects of Jet Impingement on Convective Heat Transfer in Effusion Holes,” International Gas Turbine and Aeroengine Congress and Exposition, GT2020-15577.
146 Wilkins, P. H., Lynch, S. P., Thole, K. A., Quach, S., Vincent, T., “Experimental Heat Transfer and Boundary Layer Measurements on a Ceramic Matric Composite Surface,” International Gas Turbine and Aeroengine Congress and Exposition, GT2020-15053.
145 McClain, S. T., Hanson, D. R., Cinnamon, E., Snyder, J. C., Kunz, R. F., Thole, K. A., “Flow in a Simulated Turbine Blade Cooling Channel with Spatially Varying Roughness Caused by Additive Manufacturing Orientation,” International Gas Turbine and Aeroengine Congress and Exposition, GT2020-14809.
144 Siroka, S., Berdanier, R. A., Thole, K. A., Chana, K., Haldeman, C. W., and Anthony, R. J., 2019 “Comparison of Thin Film Heat Flux Gauge Technologies Emphasizing Continuous-Duration Operation,” International Gas Turbine and Aeroengine Congress and Exposition, Phoenix, AZ, GT2019-91817.*
143 Berdanier, R. A., DeShong, E. T., Thole, K. A., 2019 “Evaluating the Effects of Transient Purge Flow on Stator-Rotor Seal Performance,” International Gas Turbine and Aeroengine Congress and Exposition, Phoenix, AZ, GT2019-91654.
142 Monge-Concepcion, I., Berdanier, R. A., Barringer, M. D., Thole, K. A., Robak, C., 2019 “Evaluating the Effect of Vane Trailing Edge Flow on Turbine Rim Sealing” International Gas Turbine and Aeroengine Congress and Exposition, Phoenix, AZ, GT2019-91576.
141 Cory, Trevor, Kirsch, K. L., Lundgreen, R., Prenter, R., Kramer, S., 2019 “Impact of Dust Feed on Capture Efficiency and Deposition Patterns in a Double-Walled Liner” International Gas Turbine and Aeroengine Congress and Exposition, Phoenix, AZ, GT2019-90981.
140 Robak, C., Faghri, A. and Thole, K. A., 2019 “Analysis of Gas Turbine Rim Cavity Ingestion with Axial Purge Flow Injection” International Gas Turbine and Aeroengine Congress and Exposition, Phoenix, AZ, GT2019-91807.
139 Hanson, D. R., McClain, S. T., Snyder, J. C., Kunz, R. F., and Thole, K. A., 2019 “Flow in a Scaled Turbine Coolant Channel with Roughness Due to Additive Manufacturing” International Gas Turbine and Aeroengine Congress and Exposition, Phoenix, AZ, GT2019-90931.
138 Snyder, J. C. and Thole, K. A., 2019 “Performance of Public Film Cooling Geometries Produced through Additive Manufacturing” International Gas Turbine and Aeroengine Congress and Exposition, Phoenix, AZ, GT2019-90877.*
137 Snyder, J. C. and Thole, K. A., 2019 “Effect of Additive Manufacturing Process Parameters on Turbine Cooling” International Gas Turbine and Aeroengine Congress and Exposition, Phoenix, AZ, GT2019-90862.*
136 Stimpson, C. K., Snyder, J. C., Thole, K. A., and Mongillo, D., 2018 “Effects of Coolant Feed Direction on Additively Manufactured Film Cooling Holes” International Gas Turbine and Aeroengine Congress and Exposition, Oslo, Norway, GT2018-77287.*
135 Shrager, A. and Thole, K. A., 2018 “Effects of Effusion Cooling Pattern Near the Dilution Hole for a Double-Walled Combustor Liner—Part 2: Flowfield Measurements,” International Gas Turbine and Aeroengine Congress and Exposition, Oslo, Norway, GT2018-77290.*
134 Shrager, A. and Thole, K. A., 2018 “Effects of Effusion Cooling Pattern Near the Dilution Hole for a Double-Walled Combustor Liner—Part 1: Overall Effectiveness Measurements,” International Gas Turbine and Aeroengine Congress and Exposition, Oslo, Norway, GT2018-77288.*
133 Berdanier, R. A., Monge-Concepcion, I., Knisely, B. F., Barringer, M., Grover, E., 2018, “Scaling Sealing Effectiveness in a Stator-Rotor Cavity for Differing Blade Spans,” International Gas Turbine and Aeroengine Congress and Exposition, Oslo, Norway, GT2018-77105.*
132 Kirsch, K. and Thole, K. A., 2018 “Numerical Optimization, Characterization, and Experimental Investigation of Additively Manufactured Communicating Microchannels,” International Gas Turbine and Aeroengine Congress and Exposition, Oslo, Norway, GT2018-75429.*
131 Kirsch, K. L., Snyder, J. C., Stimpson, C. K., Thole, K. A., and Mongillo, D., 2017, “Repeatability in Performance of Micro Cooling Geometries Manufactured with Laser Powder Bed Fusion,” 53rd AIAA/SAE/ASME Joint Propulsion Conference, Atlanta, GA, pp. 1–14. (Best Paper Award)
130 Town, J., Straub, D. Black, J., Thole, K. A., and Shih, T., 2017 “State-of-the-Art Cooling Technology for a Turbine Rotor Blade,” International Gas Turbine and Aeroengine Congress and Exposition, Charlotte, S. C., GT2017-64728.
129 Stimpson, C. K., Snyder, J. C., Thole, K. A., and Mongillo, D., 2017 “Effectiveness Measurements of Additively Manufactured Film Cooling Holes” International Gas Turbine and Aeroengine Congress and Exposition, Charlotte, S. C., GT2017-64903. *
128 Kirsch, K., and Thole, K. A., 2017 “Experimental Investigation of Numerically Optimized Wavy Microchannels Created Through Additive Manufacturing” International Gas Turbine and Aeroengine Congress and Exposition, Charlotte, S. C., GT2017-64943.*
127 Ferster, K., Kirsch, K., and Thole, K. A., 2017 “Effects of Geometry and Spacing in Additively Manufactured Microchannel Pin Fin Arrays” International Gas Turbine and Aeroengine Congress and Exposition, Charlotte, S. C., GT2017-63442.*
126 Clark, K., Barringer, M., Johnson, D., Thole, K. A., Grover, E., and Robak, C., 2017 “Effects of Purge Flow Configuration on Sealing Effectiveness in a Rotor-Stator Cavity” International Gas Turbine and Aeroengine Congress and Exposition, Charlotte, S. C., GT2017-63910.*
125 Michael Alley, Christine Haas, and Karen Thole, 2016, “Engineering Ambassadors Network: Progress in 2015 on Creating a National Network of Ambassadors,” 2016 ASEE National Conference New Orleans, LA.
124 Kirsch, K. and Thole, K.A., “Heat transfer and Pressure Loss Measurements in Additively Manufactured Wavy Microchannels,” International Gas Turbine and Aeroengine Congress and Exposition, Seoul, S. Korea, GT2016-56510.*
123 Stimpson, C., Snyder, J., Thole, K. A., and Mongillo, D., “Scaling Roughness Effects on Pressure Loss and Heat Transfer of Additively Manufactured Channels,” International Gas Turbine and Aeroengine Congress and Exposition, Seoul, S. Korea, GT2016-58093.*
122 Schroeder, R., Thole, K. A., “Effect of In-Hole Roughness on Film Cooling from a Shaped Hole,” International Gas Turbine and Aeroengine Congress and Exposition, Seoul, S. Korea, GT2016-56978.*
121 Schroeder, R., Thole, K. A., “Thermal Field Measurements for a Shaped Hole at Low and High Freestream Turbulence Intensity,” International Gas Turbine and Aeroengine Congress and Exposition, Seoul, S. Korea, GT2016-56967.*
120 Gibson, J., Thole, K. A., Christophel, J., Memory, C., Praisner, T., “ Pressure Distortion Effects on Rim Seal Performance in a Linear Cascade,” International Gas Turbine and Aeroengine Congress and Exposition, Seoul, S. Korea, GT2016-58098.
119 Clark, K., Barringer, M., Thole, K. A., Clum, C., Hiester, P., Memory, C., Robak, C., “Using a Tracer Gas to Quantify Sealing Effectiveness for Engine Realistic Rim Seals,” International Gas Turbine and Aeroengine Congress and Exposition, Seoul, S. Korea, GT2016-58095.
118 Clark, K., Barringer, M., Thole, K., Clum, C., Hiester, P., Memory, C., Robak, C., “Effects of Purge Distribution and Flowrates on Vane Rim Sealing,” International Gas Turbine and Aeroengine Congress and Exposition, Seoul, S. Korea, GT2016-58099.*
117 Michael Alley, Christine Haas, and Karen Thole, 2015, “Engineering Ambassadors Network: Progress in 2014 on Creating a National Network of Ambassadors,” 2015 ASEE National Conference. Seattle, WA.
116 Lynch, S., Thole, K. A., 2016, “Comparison of the Three-Dimensional Boundary Layer on Flat Versus Contoured Endwall,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal, Canada, GT2015-1245.*
115 Mensch, A. and Thole, K. A., “Overall Effectiveness and Flowfield Measurements for an Endwall with Non-Axisymmetric Contouring,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal, Canada, GT2015-42706.*
114 Schroeder, R. P., and Thole, K. A., “Effect of High Freestream Turbulence on Flowfields of Shaped Film Cooling Holes,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal Canada, GT2015-43339.*
113 Snyder, J., Stimpson, C., Thole, K. A., and Mongillo, D., “Build Direction Effects on Additively Manufactured Channels,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal Canada, GT2015-43935.*
112 Stimpson, C., Snyder, J., Thole, K. A., and Mongillo, D., “Roughness Effects on Flow and Heat Transfer for Additively Manufactured Channels,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal Canada, GT2015-43940.*
111 Gibson, J. and Thole, K. A., “Effects of the Main Gas Path Pressure Field on Rim Seal Flows in a Stationary Linear Cascade,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal Canada, GT2015-43517.
110 Michael Alley, Christine Haas, and Karen Thole, 2016, “Engineering Ambassadors Network: Progress in 2013 on Creating a National Network of Ambassadors,” 2014 ASEE National Conference. Indianapolis, IN.
109 Mensch, A. and Thole, K., “Simulations of Multiphase Particle Deposition on a Gas Turbine Endwall with Impingement and Film Cooling,” IMECE2014-36682. *
108 Barringer, M. D., Coward, A. C, Clark, K., Thole, K. A., Schmitz, J., Wagner, J., Alvin, M. A., Burke, P., Dennis, R., “Development of a Steady Aero Thermal Research Turbine (START) for Studying Secondary Flow Leakages and Airfoil Heat Transfer,” International Gas Turbine and Aeroengine Congress and Exposition, Dusseldorf, Germany, GT2014-25570.
107 Mensch, A., Thole, K. A., Craven, B. A., “Conjugate Heat Transfer Measurements and Predications of a Blade Endwall with a Thermal Barrier Coating,” International Gas Turbine and Aeroengine Congress and Exposition, Dusseldorf, Germany, GT2014-25436.*
106 Whitfield, C. A., Schroeder, R. P., Thole, K. A., Lewis, S. D., “Blockage Effects from Simulated Thermal Barrier Coatings for Cylindrical and Shaped Holes,” International Gas Turbine and Aeroengine Congress and Exposition, Dusseldorf, Germany, GT2014-25576.*
105 Schroeder, R. P., and Thole, K. A., “Adiabatic Effectiveness Measurements for a Baseline Shaped Film Cooling Hole,” International Gas Turbine and Aeroengine Congress and Exposition, Dusseldorf, Germany, GT2014-25992.
104 Kirsch, K. L. and Thole, K. A., “Heat Transfer Measurements of Oblong Pins,” International Gas Turbine and Aeroengine Congress and Exposition, Dusseldorf, Germany, GT2014-25370.*
103 Kirsch, K. L., Ostanek, J. K., Thole, K. A., and Kaufman, E., “Heat Transfer Measurements for Pin Fin Arrays Row Removal,” International Gas Turbine and Aeroengine Congress and Exposition, Dusseldorf, Germany, GT2014-25348.
102 Barringer, M., Thole, K. A., Krishnan, V., Landrum, E., Sanders, P., “Manufacturing Influences on Pressure Losses of Channel Fed Holes,” International Gas Turbine and Aeroengine Congress and Exposition, San Antonio, Texas, GT 2013-95236.*
101 Eberly, M. K. and Thole, K. A., “Time-Resolved Film-Cooling Flows at High and Low Density Ratios,” International Gas Turbine and Aeroengine Congress and Exposition, San Antonio, Texas, GT 2013-95031.*
100 Lynch, S. P., Thole, K. A., Kohli, A., and Lehane, C., “Endwall Heat Transfer for a Turbine Blade with an Upstream Cavity and Rim Seal Leakage,” International Gas Turbine and Aeroengine Congress and Exposition, San Antonio, Texas, GT 2013-94942.
99 Lynch, S. P., Thole, K. A., Kohli, A., and Lehane, C., “Aerodynamic Loss for a Turbine Blde with Endwall Leakage Features and Contouring,” International Gas Turbine and Aeroengine Congress and Exposition, San Antonio, Texas, GT 2013-94943.
98 Mensch, A. and Thole, K. A., “Overall Effectiveness of a Blade Endwall with Jet Impingement and Film Cooling,” International Gas Turbine and Aeroengine Congress and Exposition, San Antonio, Texas, GT 2013-94165.
97 Kirsch, K.L., Ostanek, J. K., and Thole, K. A., “Comparison of Pin Surface Heat Transfer in Arrays of Oblong and Cylindrical Pin Fins,” International Gas Turbine and Aeroengine Congress and Exposition, San Antonio, Texas, GT 2013-95146.*
96 Ostanek, J. K. and Thole, K.A., “Effects of Non-Uniform Streamwise Spacing in Low Aspect Ratio Pin Fin Arrays,” International Gas Turbine and Aeroengine Congress and Exposition, San Antonio, Texas, GT 2013-95889.*
95 Hargather, M. J., and Thole, K. A., “Characterization of Flow Through Porous Metals,” International Gas Turbine and Aeroengine Congress and Exposition, San Antonio, Texas, GT 2013-94945.
94 Hatzell, J., Marshall, M., Alley, M., Thole, K.A., Garner, J., Haas, C., Engel, R., 2013, “Engineering Ambassador Network: Professional Development Programs with an Outreach Focus,” American Society of Engineering Education Conference, Atlanta, Georgia.
93 Thole, K. A., Marshall, M., Alley, M., Zappe, S., 2013, “Engineering Ambassador Network: Dissemination through an Inaugural National Workshop,” American Society of Engineering Education Conference, Atlanta, Georgia.
92 Musgrove, G. O., Thole, K. A., Grover, E., and Barker, J., 2012, “Performance Measurements of a Unique Louver Particle Separator for Gas Turbine Engines,” International Gas Turbine and Aeroengine Congress and Exposition, Copenhagen, GT2012-69670.*
91 Ostanek, J. and Thole, K. A., 2012, “Effects of Aspect Ratio and Spacing in Pin-Fin Arrays,” International Gas Turbine and Aeroengine Congress and Exposition, Copenhagen, GT2012-68127.
90 Lawson, S., Lynch, S., and Thole, K. A., 2012, “Simulations of Multi-Phase Particle Deposition on a Non-Axisymmetric Contoured Endwall with Film-Cooling,” International Gas Turbine and Aeroengine Congress and Exposition, Copenhagen, GT2012-68174.*
89 Thrift, A. A., Thole, K. A., Hada, S., 2012, “Impact of the Combustor-Turbine Interface Slot Orientation on the Durability of a Nozzle Guide Vane Endwall,” International Gas Turbine and Aeroengine Congress and Exposition, Copenhagen, GT2012-68096.*
88 Barringer, M.D., Thole, K. A., Breneman, D. L., Tham, K-M, and Laurello, V., 2012, “Effects of Centrifugal Forces on Particle Deposition for a Representative Seal Pin Between Two Blades,” International Gas Turbine and Aeroengine Congress and Exposition, Copenhagen, GT2012-68777.*
87 Ostanek, J. and Thole, K. A., 2011, “Flowfield Measuremetns in a Single Row of Low Aspect Ratio Pin-Fins,” International Gas Turbine and Aeroengine Congress and Exposition, Vancouver, GT2011-45757.*
86 Thrift, A., Thole, K. A., and Hada, S., 2011, “Effects of Orientation and Position of the combustor-Turbine Interface Gap on the Cooling of a Vane Endwall,” International Gas Turbine and Aeroengine Congress and Exposition, Vancouver, GT2011-45507.*
85 Lawson, S. and Thole, K. A., 2011, “Simulations of Multi-Phase Particle Deposition on a Showerhead with Staggered Film-Cooling Holes,” International Gas Turbine and Aeroengine Congress and Exposition, Vancouver, GT2011-45191.*
84 Lawson, S. and Thole, K. A., 2011, “Simulations of Multi-Phase Particle Deposition on Endwall Film-Cooling Holes in Transverse Trenches,” International Gas Turbine and Aeroengine Congress and Exposition, Vancouver, GT2011-45190.*
83 Marshall, M., Alley, M., Zappe, S., Thole, K., Frecker, M., Engel, R., 2010, “Ambassador Program for Recruiting Girls into Engineering-Appropriate Messages, Messengers, and Modes of Delivery,” 40th ASEE/IEEE Frontiers in Engineering Conference, T1A, October 27-30, 2010, Washington, DC.
82 Weaver, S., Barringer, M., Thole, K. A., 2010, “Micro Channels with Manufacturing Roughness Levels,” International Gas Turbine and Aeroengine Congress and Exposition, Glasgow, GT2010-22976.*
81 Thrift, A. A., Thole, K. A., Hada, S., 2010 “Effects of an Axisymmetric Contoured Endwall on a Nozzle Guide Vane: Heat Transfer Measurements,” International Gas Turbine and Aeroengine Congress and Exposition, Glasgow, GT2010-22970.*
80 Thrift, A. A., Thole, K. A., Hada, S., 2010 “Effects of an Axisymmetric Contoured Endwall on a Nozzle Guide Vane: Adibatic Effectiveness Measurements,” International Gas Turbine and Aeroengine Congress and Exposition, Glasgow, GT2010-22968.*
79 Lawson, S. A. and Thole, K. A., 2010, “Simulations of Multi-Phase Particle Deposition on Endwall Film-Cooling,” International Gas Turbine and Aeroengine Congress and Exposition, Glasgow, GT2010-22376.*
78 Lynch, S. P., Thole, K. A., Kohli, A., Lehane, C., 2010, “Computational Predictions of Heat Transfer and Film-Cooling for a Turbine Blade with Non-Axiymmetric Endwall Contouring,” International Gas Turbine and Aeroengine Congress and Exposition, Glasgow, GT2010-22984.*
77 Lynch, S. and Thole, K. A., 2009, “The Effect of the Combustor-Turbine Slot and Mid-Passage Gap on Vane Endwall Heat Transfer,” International Mechanical Engineering Conference, Orlando, IMECE2009-12847 (recipient of the W. M. Rohsenow Prize for Best Presentation for the Gas Turbine Heat Transfer Committee).*
76 Knost, D. G., Thole, K. A., and Duggleby, A., 2009, “Evaluating a Three-Dimensional Slot Design for the Combustor-Turbine Interface,” International Gas Turbine and Aeroengine Congress and Exposition, Orlando, GT2009-60168.
75 Lawson, S. A. and Thole, K. A., 2009, “The Effects of Simulated Particle Deposition on Film Cooling,” International Gas Turbine and Aeroengine Congress and Exposition, Orlando, GT2009-59109.*
74 Cardwell, N. D., Vlachos, P. P., Thole, K. A., 2009, “A Method for Identifying and Visualizing Foreign Particle Motion Using Time Resolved Particle Tracking Velocimetry,” International Gas Turbine and Aeroengine Congress and Exposition, Orlando, GT2009-60273.*
73 Musgrove, G. O., Barringer, M.D., Thole, K. A., Grover, E., Barker, J., 2009, “Computational Design of a Louver Particle Separator for Gas Turbine Engines,” International Gas Turbine and Aeroengine Congress and Exposition, Orlando, GT2009-60199.
72 Lynch, S. P., Sundaram, N., Thole, K. A., Kohli, A., Lehane, C., 2009, “Heat Transfer for a Turbine Blade with Non-Axisymmetric Endwall Contouring,” International Gas Turbine and Aeroengine Congress and Exposition, Orlando, GT2009-60185.*
71 Cardwell, N., Vlachos, P., and Thole, K. A., 2008, “Developing and Fully Developed Turbulent Flow in Ribbed Channels,” Fluids Engineering Conference, FEDSM2008-55190 (Best Paper).
70 Ostanek, J., Thole, K. A., Prausa, J., and Van Suetendael, A., “Establishing a Methodology for Resolving Convective Heat Transfer from Complex Geometries,” International Gas Turbine and Aeroengine Congress and Exposition, Berlin, GT2008-51411.*
69 Sundaram, N. and Thole, K. A., “Film-Cooling Flowfields with Trenched Holes on an Endwall,” International Gas Turbine and Aeroengine Congress and Exposition, Berlin, GT2008-50149.*
68 Colban, W., Thole, K. A., Bogard, D., “A Film Cooling Correlation for Shaped Holes on a Flat-Plate Surface,” International Gas Turbine and Aeroengine Congress and Exposition, Berlin, GT2008-50121.*
67 Land, C., Thole, K. A., Joe, C., “Considerations of a Double-Wall Cooling Design to Reduce Sand Blockage,” International Gas Turbine and Aeroengine Congress and Exposition, Berlin, GT2008-50160.*
66 Cardwell, N., Thole, K. A., Burd, S., “Investigation of Sand Blocking within Impingement and Film-Cooling Holes,” International Gas Turbine and Aeroengine Congress and Exposition, Berlin, GT2008-51351.*
65 Nasir, S., Carullo, J., Ng, W., Thole, K., Wu, H., Moon, H. K., “Effects of Large Scale High Freestream Turbulence, and Exit Reynolds Number on Turbine Vane Heat Transfer in a Transonic Cascade,” International Mechanical Engineering Congress, Seattle, IMECE 2007-44098.*
64 Barringer, M.D., Thole, K. A., Polanka, M. D., Clark, J. P., and Koch, P. J., “Migration of Combustor Exit Profiles Through High Pressure Turbine Vanes,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal, GT2007-27157.*
63 Barringer, M. D., Thole, K. A., and Polanka, M.D., “An Experimental Study of Combustor Exit Profile Shapes on Endwall Heat Transfer in High Pressure Turbine Vanes,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal, GT2007-27156.*
62 Sundaram, N. and Thole, K. A., “Bump and Trench Modifications to Film-Cooling Holes at the Vane Endwall Junction,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal, GT2007-27132.*
61 Sundaram, N., Barringer, M. D., and Thole, K. A., “Effects of Deposits on Film Cooling of a Vane Endwall Along the Pressure Side,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal, GT2007-27131.*
60 Lynch, S. P. and Thole, K. A., “The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal, GT2007-27867.*
59 Lyall, M. E., Thrift, A. A., Thole, K. A., and Kohli, A., “Heat Transfer from Low Aspect Ratio Pin Fins,” International Gas Turbine and Aeroengine Congress and Exposition, Montreal, GT2007-27431.*
58 Hada, S. and Thole, K. A., “Effect of the Midpassage Gap Leakage on the Turbine Endwall,” Eleventh International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Hawaii, March 2006.*
57 Hada, S. and Thole, K. A., “Computational Study of a Midpassage Gap and Upstream Slot on Vane Endwall Film-Cooling,” International Gas Turbine and Aeroengine Congress and Exposition, Barcelona, GT2006-91067.*
56 Walsh, S., Thole, K. A., and Joe, C., “Effects of Sand Ingestion on the Blockage of Film-Cooling Holes,” International Gas Turbine and Aeroengine Congress and Exposition, Barcelona, GT2006-90067.
55 Scrittore, J., Thole, K. A., and Burd, S., “Investigation of Velocity Profiles for Effusion Cooling of a Combustor Liner,” International Gas Turbine and Aeroengine Congress and Exposition, Barcelona, GT2006-90532.*
54 Barringer, M., Thole, K. A., and Polanka, M., “Experimental Evaluation of an Inlet Profile Generator for High Pressure Turbine Tests,” International Gas Turbine and Aeroengine Congress and Exposition, Barcelona, GT2006-
90401.*
53 Barringer, M., Thole, K. A., and Polanka, M. D., “Effects of Combustor Exit Profiles on High Pressure Turbine Vane Aerodynamics and Heat Transfer,” International Gas Turbine and Aeroengine Congress and Exposition, Barcelona,
GT2006-90277.*
52 Kunze, V., Wolff, M., Barringer, M., Thole, K. A., Polanka, M., “Numerical Insight into Flow and Thermal Patterns within an Inlet Profile Generator Comparing to Experimental Results,” International Gas Turbine and Aeroengine Congress and Exposition, Barcelona, GT2006-90276.
51 Cardwell, N., Narayan, S., and Thole, K. A. “The Effects of Varying the Combustor-Turbine Gap,” International Gas Turbine and Aeroengine Congress and Exposition, Barcelona, GT2006-90089.*
50 Colban, W., Thole, K. A., and Haendler, M., “A Comparison of Cylindrical and Fan-Shaped Film-Cooling Holes on a Vane Endwall at Low and High Freestream Turbulence Levels,” International Gas Turbine and Aeroengine Congress and Exposition, Barcelona, GT2006-90021.*
49 Narayan, S. and Thole, K. A. “Effects of Surface Deposition, Hole Blockage, and TBC Spallation on Vane Endwall Film-Cooling,” GT2006-90379.*
48 Colban, W., Thole, K. A., and Haendler, M., “Experimental and Computational Comparisons of Fan-Shaped Film-Cooling on a Turbine Vane Surface,” International Mechanical Engineering Congress, Orlando, IMECE2005-79596, recipient of the W. M. Rohsenow Prize for Best Presentation for the Gas Turbine Heat Transfer Committee.*
47 V. R. Kunze and M. Wolff M. D. Barringer and K. A. Thole M. D. Polanka, “Numerical Modeling of Flow and Thermal Patterns Within a Combustor Simulator,” International Gas Turbine and Aeroengine Congress and Exposition, Reno, GT2005-68284.
46 Scrittore, J., Thole, K. A., and Burd, S., “Experimental Characterization of Film-Cooling Effectiveness Near Combustor Dilution Holes,” International Gas Turbine and Aeroengine Congress and Exposition, Reno, GT2005-68704.*
45 Colban, W., Thole, K. A., and Haendler, M., “Heat Transfer and Film-Cooling Measurements on a Stator Vane with Fan-Shaped Cooling Holes,” International Gas Turbine and Aeroengine Congress and Exposition, Reno, GT2005-68258. *
44 Cardwell, N., Sundaram, N., and Thole, K. A., “Effects of Roughness and Mid-Passage Gap on Endwall Film
Cooling,” International Gas Turbine and Aeroengine Congress and Exposition, Reno, GT2005-68704.*
43 Ranson, W., Thole, K. A., and Cunha, F. “Adiabatic Effectiveness Measurements and Predictions of Leakage Flows Along a Blade Endwall,” International Mechanical Engineering Congress, Anaheim, IMECE2004-62021.*
42 Kunze, V. R., Wolff, M., Barringer, M., Thole, K., and Polanka, M., “Developing a Combustor Simulator for Investigating High Pressure Turbine Aerodynamics and Heat Transfer,” International Gas Turbine and Aeroengine Congress and Exposition, Vienna, GT2004-53613.
41 Christophel, J. R., Thole, K., and Cunha, F, “Cooling the Tip of a Turbine Blade Using Pressure Side Holes-Part 2: Heat Transfer Measurements,” International Gas Turbine and Aeroengine Congress and Exposition, Vienna, GT2004-53254.*
40 Christophel, J. R., Thole, K., and Cunha, F, “Cooling the Tip of a Turbine Blade Using Pressure Side Holes-Part 1: Film Effectiveness Measurements,” International Gas Turbine and Aeroengine Congress and Exposition, Vienna, GT2004-53251.*
39 Christophel, J. R., Couch, E., Thole, K., and Cunha, F., “Measured Adiabatic Effectiveness and Heat Transfer for Blowing from the Tip of a Turbine Blade,” International Gas Turbine and Aeroengine Congress and Exposition, Vienna, GT2004-53250.*
38 Knost, D. G., and Thole, K. A., “Adiabatic Effectiveness Measurements of Endwall Film-Cooling for a First Stage Vane,” International Gas Turbine and Aeroengine Congress and Exposition, Vienna, GT2004-52236.
37 Graham, A., and Thole, K. A., “Flowfield Measurements in a Ribbed Channel Relevant to Internal Turbine Blade Cooling,” International Gas Turbine and Aeroengine Congress and Exposition, International Gas Turbine and Aeroengine Congress and Exposition, Vienna, GT2004-53361.
36 Smith, A. C., Hatchett, J. H., Nix, A. C., Ng, W. F., and Thole, K. A., “Effectiveness of Normal and Angled Slot Cooling,” International Gas Turbine and Aeroengine Congress and Exposition, Vienna, GT2004-53248.
35 Vakil, S. and Thole, K. A., 2003, “Flow and Thermal Field Measurements in a Combustor Simulator Relevant to a Gas Turbine Aero-Engine,” International Gas Turbine and Aeroengine Congress and Exposition, Atlanta, GT-2003-38254.*
34 Lethander, A., Thole, K. A., Zess, G., and Wagner, J., “Optimizing the Vane-Endwall Junction to Reduce Adiabatic Wall Temperatures in a Turbine Vane Passage,” International Gas Turbine and Aeroengine Congress and Exposition, Atlanta, GT-2003-38940.*
33 Stitzel, S. and Thole, K. A., 2003, “Flow Field Computations of Combustor-Turbine Interactions Relevant to a Gas Turbine Engine,” International Gas Turbine and Aeroengine Congress and Exposition, Atlanta, GT-2003-38253.*
32 Knost, D. and Thole, K. A., 2003, “Computational Predictions of Endwall Film-Cooling for a First Stage Vane,” International Gas Turbine and Aeroengine Congress and Exposition, Atlanta, GT-2003-38252.
31 Hohlfeld, E., Couch, E., Christophel, J. and Thole, K. A., 2003, “Predictions of Cooling from Dirt Purge Holes Along the Tip of a Turbine Blade,” International Gas Turbine and Aeroengine Congress and Exposition, Atlanta, GT-2003-38251. *
30 Pang, Y. F., Chen, J. Z., Scott, E. P., and Thole, K. A., 2002, “Electrical and Thermal Layout Design and Optimization Considerations for DPS Active IPEM,” New Orleans, IMECE2002-33778.
29 Nix, A., Smith, A. C., Diller, T. E., Ng, W. F., and Thole, K. A., 2002, “High Intensity, Large Length Scale, Freestream Turbulence Generation in a Transonic Turbine Cascade,” International Gas Turbine and Aeroengine Congress and Exposition, Amsterdam, ASME Paper GT-2002-30523.
28 Hermanson, K. and Thole, K. A., 2002, “Effect on Non-Uniform Inlet Conditions on Endwall Secondary Flows,” International Gas Turbine and Aeroengine Congress and Exposition, Amsterdam, GT-2002-30188.*
27 Colban, W. F., Lethander, A., T., Thole, K. A., and Zess, G., 2002, “Combustor-Turbine Interface Studies: Part 2: Flow and Thermal Field Measurements,” International Gas Turbine and Aeroengine Congress and Exposition, Amsterdam, GT-2002-30527.*
26 Colban, W. F., Thole, K. A., and Zess, G., 2002, “Combustor-Turbine Interface Studies: Part 1: Endwall Measurements,” International Gas Turbine and Aeroengine Congress and Exposition, Amsterdam, GT-2002-30526.*
25 Harrington, M., McWaters, M., Bogard, D., Lemmon, C., and Thole, K. A. “Full-Coverage Film Cooling with Short Normal Injection Holes,” International Gas Turbine and Aeroengine Congress and Exposition, New Orleans, 2001-GT-0130.*
24 Radomsky, R. and Thole, K. A., 2001, “Detailed Boundary Layer Measurements on a Turbine Stator Vane at Elevated Freestream Turbulence Levels,” International Gas Turbine and Aeroengine Congress and Exposition, New Orleans, 2001-GT-0169.*
23 Barringer, M. D., Richard, O. T., Walter, J. P., Stitzel, S. M., and Thole, K. A., 2001, “Flow Field Simulations of a Gas Turbine Combustor,” International Gas Turbine and Aeroengine Congress and Exposition, New Orleans, 2001-GT-0170.
22 Zess, G. A. and Thole, K. A., 2001, “Computational Design and Experimental Evaluation of Using a Leading Edge Fillet on a Gas Turbine Vane,” International Gas Turbine and Aeroengine Congress and Exposition, New Orleans, 2001-GT-0404.*
21 Thole, K. A., Radomsky, R., Kang, M., and Kohli, A., 2001, “Elevated Freestream Turbulence Effects on Heat Transfer for a Gas Turbine Vane,” Turbulent Heat Transfer Conference, Anchorage, AK, March.
20 Radomsky, R., and Thole, K. A., 2000, “High Freestream Turbulence Effects in the Endwall Leading Edge Region,” International Gas Turbine and Aeroengine Congress and Exposition, Munich Germany, 2000-GT-201.*
19 Lemmon, C., Kohli, A., and Thole, K. A., 1999, “Formation of Counter-Rotating Vortices in Film-Cooling
Flows,” International Gas Turbine and Aeroengine Congress and Exposition, Indianapolis Indiana, 99-GT-161.
18 Radomsky, R. and Thole, K. A., 1999, “Highly Turbulent Flowfield Measurements Around a Stator Vane,” International Gas Turbine and Aeroengine Congress and Exposition, Indianapolis Indiana, 99-GT-253.*
17 Kang, M., and Thole, K. A., 1999, “Flowfield Measurements in the Endwall Region of a Stator Vane,” International Gas Turbine and Aeroengine Congress and Exposition, Indianapolis Indiana, 99-GT-188.*
16 Zhang, L. W., Memory, S. B., Wattelet, J. P., Springer, M.E., and Thole, K. A., 1999, “A Combined Experimental and Computational Study of Flowfields in a Louvered Fin Heat Exchanger,” VTMS 4, ICE, London United Kingdom.
15 Hermanson, K. and Thole, K.A., 1999, “Effect of Inlet Conditions on Endwall Secondary Flows,” AIAA Aerospace Meeting, Reno Nevada, AIAA Paper 99-0241.
14 Springer, M., and Thole, K. A., Zhang, L. W., Memory, S. B., and Wattelet, J. P., Modine Manufacturing, 1998, “A Combined CFD and LDV Study of Flowfields in Louvered Fin Heat Exchangers,” ASME Fluids Engineering Division Meeting, Paper Number FEDSM98-4843.
13 Kohli, A., and Thole, K. A., 1998, “Entrance Effects on a Diffused Film-Cooling Hole,” International Gas Turbine and Aeroengine Congress and Exposition, Stockholm Sweden, 98-GT-402.
12 Kang, M., Kohli, A., and Thole, K. A., 1998, “Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall,” International Gas Turbine and Aeroengine Congress and Exposition, Stockholm Sweden,
98-GT-173.*
11 Radomsky, R., and Thole, K. A., 1998, “Effects of High Freestream Turbulence Levels and Length Scales on Stator Vane Heat Transfer,” International Gas Turbine and Aeroengine Congress and Exposition, Stockholm Sweden, 98-GT-236.
10 Kohli, A., and Thole, K. A., 1997, “A CFD Investigation on the Effect of Entrance Flow Conditions in Discrete Film Cooling Holes,” 32nd National Heat Transfer Conference, vol. 12, pp. 223-232, W. M. Rohsenow Prize for Best Presentation for the Gas Turbine Heat Transfer Committee.
9 Martin, C., and Thole, K. A., 1997, “A CFD Benchmark Study: Leading Edge Film Cooling with Compound Angle Injection,” presented to The International Gas Turbine and Aeroengine Congress and Exposition, Orlando, Florida, 97-GT-297.
8 Bangert, B., Kohli, A., Sauer, J., and Thole, K. A., 1997, “High Freestream Turbulence Simulation in a Scaled-Up Turbine Vane Passage,” International Gas Turbine and Aeroengine Congress and Exposition, Orlando, Florida, 97-GT-51.
7 Thole, K. A., Gritsch, M., Schulz, A., and Wittig, S., 1996, “Flowfield Measurements for Cooling Holes with Expanded Exits,” International Gas Turbine and Aeroengine Congress and Exposition, Birmingham England, 96-GT-174.*
6 Wittig, S., Schulz, A., Gritsch, M., and Thole, K. A., 1996, “Transonic Film Cooling Investigations: Effects of Hole Shapes and Orientations,” International Gas Turbine and Aeroengine Congress and Exposition, Birmingham England, 96-GT-222.*
5 Laudon, M. F., Engelstad, R. L., Thole, K. A., Dauksher, W. J., Resnick, D. J., Cummings, K. D., and Seese, P. and Johnson, W., 1995, “Modeling of In-Plane Distortions due to Variations in Absorber Stress,” International Micro- and Nano- Engineering, Aix-en-Provence France.
4 Laudon, M. F., Thole, K. A., Engelstad, R. L., Resnick, D. J., Cummings, K. D., and Dauksher, W. J., 1995, “Thermal Analysis of X-ray Membrane in a Plasma Environment,” 39th International Conference on Electron, Ion and Photon Beam Technology and Nanofabrication, Phoenix Arizona.
3 Thole, K. A., and Bogard, D. G., 1994, “Enhanced Heat Transfer and Skin Friction due to High Freestream
Turbulence,” International Gas Turbine and Aeroengine Congress and Exposition, The Hague Netherlands 94-GT-296.*
2 Thole, K. A., Whan-Tong, J., and Bogard, D. G., 1991, “Generation of Very High Freestream Turbulence Levels and the Effects on Heat Transfer,” 27.5.1-27.5.7, Turbulent Shear Flow Conference, Munich, Germany.
1 Thole, K. A., Sinha, A., Bogard, D. G., and Crawford, M. E., 1990, “Mean Temperature Measurements of Jets with a Crossflow for Gas Turbine Film Cooling Application,” Rotating Machinery Transport Phenomena, J. H. Kim and W. J. Yang, ed. Hemisphere Publishing Corporation, New York, New York.