Year |
Citation |
Score |
2020 |
Berdanier RA, DeShong E, Thole KA, Robak C. Evaluating the Effects of Transient Purge Flow on Stator-Rotor Seal Performance Journal of Turbomachinery-Transactions of the Asme. 1-55. DOI: 10.1115/1.4048023 |
0.392 |
|
2020 |
Monge-Concepción I, Berdanier RA, Barringer MD, Thole KA, Robak C. Evaluating the Effect of Vane Trailing Edge Flow on Turbine Rim Sealing Journal of Turbomachinery-Transactions of the Asme. 142. DOI: 10.1115/1.4047611 |
0.415 |
|
2020 |
Snyder JC, Thole KA. Tailoring Surface Roughness Using Additive Manufacturing to Improve Internal Cooling Journal of Turbomachinery-Transactions of the Asme. 142. DOI: 10.1115/1.4047380 |
0.307 |
|
2020 |
Snyder JC, Thole KA. Performance of Public Film Cooling Geometries Produced Through Additive Manufacturing Journal of Turbomachinery-Transactions of the Asme. 142. DOI: 10.1115/1.4046488 |
0.388 |
|
2020 |
Snyder JC, Thole KA. Effect of Additive Manufacturing Process Parameters on Turbine Cooling Journal of Turbomachinery-Transactions of the Asme. 142. DOI: 10.1115/1.4046459 |
0.314 |
|
2020 |
Siroka S, Berdanier RA, Thole KA, Chana K, Haldeman CW, Anthony RJ. Comparison of Thin Film Heat Flux Gauge Technologies Emphasizing Continuous-Duration Operation Journal of Turbomachinery-Transactions of the Asme. 142: 91001. DOI: 10.1115/1.4045991 |
0.795 |
|
2019 |
Berdanier RA, Monge-Concepción I, Knisely BF, Barringer MD, Thole KA, Grover EA. Scaling Sealing Effectiveness in a Stator–Rotor Cavity for Differing Blade Spans Journal of Turbomachinery-Transactions of the Asme. 141: 51007. DOI: 10.1115/1.4042423 |
0.734 |
|
2018 |
Stimpson CK, Snyder JC, Thole KA, Mongillo D. Effects of Coolant Feed Direction on Additively Manufactured Film Cooling Holes Journal of Turbomachinery-Transactions of the Asme. 140: 111001. DOI: 10.1115/1.4041374 |
0.416 |
|
2018 |
Shrager AC, Thole KA, Mongillo D. 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-Transactions of the Asme. 141: 11023. DOI: 10.1115/1.4041153 |
0.378 |
|
2018 |
Shrager AC, Thole KA, Mongillo D. 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-Transactions of the Asme. 141: 11022. DOI: 10.1115/1.4041148 |
0.382 |
|
2018 |
Town J, Straub D, Black J, Thole KA, Shih TI. State-Of-The-Art Cooling Technology For A Turbine Rotor Blade Journal of Turbomachinery-Transactions of the Asme. 140: 71007. DOI: 10.1115/1.4039942 |
0.309 |
|
2018 |
Stimpson CK, Snyder JC, Thole KA, Mongillo D. Effectiveness Measurements of Additively Manufactured Film Cooling Holes Journal of Turbomachinery-Transactions of the Asme. 140: 11009. DOI: 10.1115/1.4038182 |
0.41 |
|
2018 |
Ferster KK, Kirsch KL, Thole KA. Effects of Geometry, Spacing, and Number of Pin Fins in Additively Manufactured Microchannel Pin Fin Arrays Journal of Turbomachinery-Transactions of the Asme. 140: 11007. DOI: 10.1115/1.4038179 |
0.307 |
|
2018 |
Kirsch KL, Thole KA. Isolating the effects of surface roughness versus wall shape in numerically optimized, additively manufactured micro cooling channels Experimental Thermal and Fluid Science. 98: 227-238. DOI: 10.1016/J.Expthermflusci.2018.05.030 |
0.323 |
|
2017 |
Clark K, Barringer MD, Johnson DK, Thole KA, Grover E, Robak C. Effects of Purge Flow Configuration on Sealing Effectiveness in a Rotor–Stator Cavity Journal of Engineering For Gas Turbines and Power-Transactions of the Asme. 140: 112502. DOI: 10.1115/1.4040308 |
0.741 |
|
2017 |
Kirsch KL, Thole KA. Heat transfer and pressure loss measurements in additively manufactured wavy microchannels Journal of Turbomachinery. 139. DOI: 10.1115/1.4034342 |
0.47 |
|
2017 |
Kirsch KL, Thole KA. Pressure loss and heat transfer performance for additively and conventionally manufactured pin fin arrays International Journal of Heat and Mass Transfer. 108: 2502-2513. DOI: 10.1016/J.Ijheatmasstransfer.2017.01.095 |
0.445 |
|
2016 |
Schroeder RP, Thole KA. Effect of in-hole roughness on film cooling from a shaped hole Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/1.4034847 |
0.447 |
|
2016 |
Schroeder RP, Thole KA. Thermal field measurements for a shaped hole at low and high freestream turbulence intensity Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/1.4034798 |
0.425 |
|
2016 |
Stimpson CK, Snyder JC, Thole KA, Mongillo D. Scaling roughness effects on pressure loss and heat transfer of additively manufactured channels Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/1.4034555 |
0.51 |
|
2016 |
Clark K, Barringer M, Thole KA, Clum C, Hiester P, Memory C, Robak C. Effects of Purge Jet Momentum on Sealing Effectiveness Journal of Engineering For Gas Turbines and Power-Transactions of the Asme. 139: 10. DOI: 10.1115/1.4034545 |
0.721 |
|
2016 |
Schroeder RP, Thole KA. Effect of high freestream turbulence on flowfields of shaped film cooling holes Journal of Turbomachinery. 138. DOI: 10.1115/1.4032736 |
0.497 |
|
2016 |
Snyder JC, Stimpson CK, Thole KA, Mongillo D. Build direction effects on additively manufactured channels Journal of Turbomachinery. 138. DOI: 10.1115/1.4032168 |
0.43 |
|
2016 |
Stimpson CK, Snyder JC, Thole KA, Mongillo D. Roughness effects on flow and heat transfer for additively manufactured channels Journal of Turbomachinery. 138. DOI: 10.1115/1.4032167 |
0.488 |
|
2016 |
Lynch SP, Thole KA. Comparison of the three-dimensional boundary layer on flat versus contoured turbine endwalls Journal of Turbomachinery. 138. DOI: 10.1115/1.4032165 |
0.719 |
|
2016 |
Mensch A, Thole KA. Overall effectiveness and flowfield measurements for an endwall with nonaxisymmetric contouring Journal of Turbomachinery. 138. DOI: 10.1115/1.4031962 |
0.856 |
|
2016 |
Lieuwen TC, Thole KA. At the Intersection Mechanical Engineering. 138: 34-37. DOI: 10.1115/1.2016-Jun-2 |
0.36 |
|
2016 |
Mensch AE, Thole KA. Effects of non-axisymmetric endwall contouring and film cooling on the passage flowfield in a linear turbine cascade Experiments in Fluids. 57: 1-16. DOI: 10.1007/S00348-015-2093-5 |
0.482 |
|
2015 |
Stimpson CK, Snyder JC, Thole KA, Mongillo D. Roughness effects on flow and heat transfer for additively manufactured channels Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/GT2015-43940 |
0.388 |
|
2015 |
Snyder JC, Stimpson CK, Thole KA, Mongillo D. Build direction effects on additively manufactured channels Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/GT2015-43935 |
0.321 |
|
2015 |
Mensch A, Thole KA. Overall effectiveness and flowfield measurements for an endwall with Non-Axisymmetric contouring Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/GT2015-42706 |
0.51 |
|
2015 |
Lynch SP, Thole KA. Heat transfer and film cooling on a contoured blade endwall with platform gap leakage Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/1.4035202 |
0.792 |
|
2015 |
Whitfield CA, Schroeder RP, Thole KA, Lewis SD. Blockage effects from simulated thermal barrier coatings for cylindrical and shaped cooling holes Journal of Turbomachinery. 137. DOI: 10.1115/1.4029879 |
0.509 |
|
2015 |
Kirsch KL, Thole KA. Heat transfer measurements of oblong pins Journal of Turbomachinery. 137. DOI: 10.1115/1.4029124 |
0.493 |
|
2015 |
Mensch A, Thole KA. Conjugate heat transfer analysis of the effects of impingement channel height for a turbine blade endwall International Journal of Heat and Mass Transfer. 82: 66-77. DOI: 10.1016/J.Ijheatmasstransfer.2014.10.076 |
0.845 |
|
2014 |
Schroeder RP, Thole KA. Adiabatic effectiveness measurements for a baseline shaped film cooling hole Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/GT2014-25992 |
0.319 |
|
2014 |
Barringer M, Coward A, Clark K, Thole KA, Schmitz J, Wagner J, Alvin MA, Burke P, Dennis R. The design of a steady aero thermal research turbine (START) for studying secondary flow leakages and airfoil heat transfer Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/GT2014-25570 |
0.397 |
|
2014 |
Kirsch KL, Ostanek JK, Thole KA, Kaufman E. Row removal heat transfer study for pin fin arrays Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/GT2014-25348 |
0.325 |
|
2014 |
Mensch A, Thole KA. Simulations of multiphase particle deposition on a gas turbine endwall with impingement and film cooling Asme International Mechanical Engineering Congress and Exposition, Proceedings (Imece). 8. DOI: 10.1115/1.4031177 |
0.832 |
|
2014 |
Mensch A, Thole KA, Craven BA. Conjugate heat transfer measurements and predictions of a blade endwall with a thermal barrier coating Proceedings of the Asme Turbo Expo. 5. DOI: 10.1115/1.4028233 |
0.839 |
|
2014 |
Mensch A, Thole KA. Overall effectiveness of a blade endwall with jet impingement and film cooling Journal of Engineering For Gas Turbines and Power. 136. DOI: 10.1115/1.4025835 |
0.843 |
|
2013 |
Lynch SP, Thole KA, Kohli A, Lehane C, Praisner T. Endwall heat transfer for a turbine blade with an upstream cavity and rim seal leakage Proceedings of the Asme Turbo Expo. 3. DOI: 10.1115/GT2013-94942 |
0.397 |
|
2013 |
Eberly MK, Thole KA. Time-resolved film-cooling flows at high and low density ratios Proceedings of the Asme Turbo Expo. 3. DOI: 10.1115/1.4025574 |
0.494 |
|
2013 |
Barringer M, Thole KA, Krishnan V, Landrum E. Manufacturing influences on pressure losses of channel fed holes Proceedings of the Asme Turbo Expo. 3. DOI: 10.1115/1.4025226 |
0.375 |
|
2013 |
Kirsch KL, Ostanek JK, Thole KA. Comparison of pin surface heat transfer in arrays of oblong and cylindrical pin fins Proceedings of the Asme Turbo Expo. 3. DOI: 10.1115/1.4025213 |
0.49 |
|
2013 |
Barringer MD, Thole KA, Breneman DL, Tham KM, Laurello V. Effects of centrifugal forces on particle deposition for a representative seal pin between two blades Journal of Engineering For Gas Turbines and Power. 135. DOI: 10.1115/1.4007751 |
0.431 |
|
2013 |
Lawson SA, Lynch SP, Thole KA. Simulations of multiphase particle deposition on a nonaxisymmetric contoured endwall with film-cooling Journal of Turbomachinery. 135. DOI: 10.1115/1.4007598 |
0.741 |
|
2013 |
Musgrove GO, Thole KA, Grover E, Barker J. Performance measurements of a unique louver particle separator for gas turbine engines Journal of Engineering For Gas Turbines and Power. 135. DOI: 10.1115/1.4007568 |
0.423 |
|
2012 |
Ostanek JK, Thole KA. Effects of varying streamwise and spanwise spacing in pin-fin arrays Proceedings of the Asme Turbo Expo. 4: 45-57. DOI: 10.1115/GT2012-68127 |
0.4 |
|
2012 |
Thrift AA, Thole KA, Hada S. Impact of the combustor-turbine interface slot orientation on the durability of a nozzle guide vane endwall Proceedings of the Asme Turbo Expo. 4: 31-43. DOI: 10.1115/1.4007602 |
0.709 |
|
2012 |
Thrift AA, Thole KA, Hada S. Effects of orientation and position of the combustor-turbine interface on the cooling of a vane endwall Journal of Turbomachinery. 134. DOI: 10.1115/1.4004817 |
0.494 |
|
2012 |
Lawson SA, Thole KA, Okita Y, Nakamata C. Simulations of Multiphase Particle Deposition on a Showerhead With Staggered Film-Cooling Holes Journal of Turbomachinery. 134. DOI: 10.1115/1.4004757 |
0.433 |
|
2012 |
Lawson SA, Thole KA. Simulations of Multiphase Particle Deposition on Endwall Film-Cooling Holes in Transverse Trenches Journal of Turbomachinery. 134. DOI: 10.1115/1.4004756 |
0.429 |
|
2012 |
Ostanek JK, Thole KA. Flowfield Measurements in a Single Row of Low Aspect Ratio Pin Fins Journal of Turbomachinery. 134. DOI: 10.1115/1.4004755 |
0.521 |
|
2012 |
Lawson SA, Thole KA. Simulations of Multiphase Particle Deposition on Endwall Film-Cooling Journal of Turbomachinery-Transactions of the Asme. 134: 11003. DOI: 10.1115/1.4002962 |
0.371 |
|
2012 |
Thrift AA, Thole KA. Influence of flow injection angle on a leading-edge horseshoe vortex International Journal of Heat and Mass Transfer. 55: 4651-4664. DOI: 10.1016/J.Ijheatmasstransfer.2012.04.024 |
0.435 |
|
2012 |
Ostanek JK, Thole KA. Effect of streamwise spacing on periodic and random unsteadiness in a bundle of short cylinders confined in a channel Experiments in Fluids. 53: 1779-1796. DOI: 10.1007/S00348-012-1394-1 |
0.454 |
|
2012 |
Ostanek JK, Thole KA. Wake development in staggered short cylinder arrays within a channel Experiments in Fluids. 53: 673-697. DOI: 10.1007/S00348-012-1313-5 |
0.459 |
|
2011 |
Ostanek JK, Thole KA. Flowfield measurements in a single row of low aspect ratio pin-fins Proceedings of the Asme Turbo Expo. 5: 1293-1304. DOI: 10.1115/GT2011-45757 |
0.426 |
|
2011 |
Lawson SA, Thole KA, Okita Y, Nakamata C. Simulations of multi-phase particle deposition on a showerhead with staggered film-cooling holes Proceedings of the Asme Turbo Expo. 5: 91-103. DOI: 10.1115/GT2011-45191 |
0.323 |
|
2011 |
Lawson SA, Thole KA. Simulations of multi-phase particle deposition on endwall film-cooling holes in transverse trenches Proceedings of the Asme Turbo Expo. 5: 79-90. DOI: 10.1115/GT2011-45190 |
0.318 |
|
2011 |
Weaver SA, Barringer MD, Thole KA. Microchannels with manufacturing roughness levels Journal of Turbomachinery. 133. DOI: 10.1115/1.4002991 |
0.47 |
|
2011 |
Thrift AA, Thole KA, Hada S. Effects of an axisymmetric contoured endwall on a nozzle guide vane: Adiabatic effectiveness measurements Journal of Turbomachinery. 133. DOI: 10.1115/1.4002965 |
0.536 |
|
2011 |
Lynch SP, Thole KA, Kohli A, Lehane C. Computational predictions of heat transfer and film-cooling for a turbine blade with nonaxisymmetric endwall contouring Journal of Turbomachinery. 133. DOI: 10.1115/1.4002951 |
0.845 |
|
2011 |
Lynch SP, Thole KA. The effect of the combustor-turbine slot and midpassage gap on vane endwall heat transfer Journal of Turbomachinery. 133. DOI: 10.1115/1.4002950 |
0.778 |
|
2011 |
Colban WF, Thole KA, Bogard D. A film-cooling correlation for shaped holes on a flat-plate surface Journal of Turbomachinery. 133. DOI: 10.1115/1.4002064 |
0.74 |
|
2011 |
Carullo JS, Nasir S, Cress RD, Ng WF, Thole KA, Zhang LJ, Moon HK. The effects of freestream turbulence, turbulence length scale, and exit reynolds number on turbine blade heat transfer in a transonic cascade Journal of Turbomachinery. 133. DOI: 10.1115/1.4001366 |
0.559 |
|
2011 |
Hada S, Thole KA. Computational study of a midpassage gap and upstream slot on vane endwall film-cooling Journal of Turbomachinery. 133. DOI: 10.1115/1.4001135 |
0.523 |
|
2011 |
Lawson SA, Thole KA. Effects of simulated particle deposition on film cooling Journal of Turbomachinery. 133. DOI: 10.1115/1.4000571 |
0.47 |
|
2011 |
Lynch SP, Sundaram N, Thole KA, Kohli A, Lehane C. Heat transfer for a turbine blade with nonaxisymmetric endwall contouring Journal of Turbomachinery. 133. DOI: 10.1115/1.4000542 |
0.829 |
|
2011 |
Lyall ME, Thrift AA, Thole KA, Kohli A. Heat transfer from low aspect ratio pin fins Journal of Turbomachinery. 133. DOI: 10.1115/1.2812951 |
0.837 |
|
2011 |
Cardwell ND, Vlachos PP, Thole KA. A multi-parametric particle-pairing algorithm for particle tracking in single and multiphase flows Measurement Science and Technology. 22. DOI: 10.1088/0957-0233/22/10/105406 |
0.775 |
|
2011 |
Lawson SA, Thrift AA, Thole KA, Kohli A. Heat transfer from multiple row arrays of low aspect ratio pin fins International Journal of Heat and Mass Transfer. 54: 4099-4109. DOI: 10.1016/J.Ijheatmasstransfer.2011.04.001 |
0.827 |
|
2011 |
Cardwell ND, Vlachos PP, Thole KA. Developing and fully developed turbulent flow in ribbed channels Experiments in Fluids. 50: 1357-1371. DOI: 10.1007/S00348-010-0993-Y |
0.827 |
|
2010 |
Lynch SP, Thole KA. The effect of the combustor-turbine slot and mid-passage gap on vane endwall heat transfer Asme International Mechanical Engineering Congress and Exposition, Proceedings. 9: 2167-2178. DOI: 10.1115/IMECE2009-12847 |
0.488 |
|
2010 |
Lynch SP, Thole KA, Kohli A, Lehane C. Computational predictions of heat transfer and film-cooling for a turbine blade with non-axisymmetric endwall contouring Proceedings of the Asme Turbo Expo. 4: 1641-1653. DOI: 10.1115/GT2010-22984 |
0.484 |
|
2010 |
Weaver SA, Barringer MD, Thole KA. Micro channels with manufacturing roughness levels Proceedings of the Asme Turbo Expo. 4: 413-422. DOI: 10.1115/GT2010-22976 |
0.313 |
|
2010 |
Thrift AA, Thole KA, Hada S. Effects of an axisymmetric contoured endwall on a nozzle guide vane: Adiabatic effectivness measurements Proceedings of the Asme Turbo Expo. 4: 1617-1627. DOI: 10.1115/GT2010-22968 |
0.445 |
|
2010 |
Thrift AA, Thole KA, Hada S. Effects of an axisymmetric contoured endwall on a nozzle guide vane: Convective heat transfer measurements Proceedings of the Asme Turbo Expo. 4: 1629-1640. DOI: 10.1115/1.4002966 |
0.539 |
|
2010 |
Thrift AA, Brumbaugh SJ, Thole KA, Kohli A. A methodology to measure aerodynamic forces on cylinders in channel flow Journal of Fluids Engineering, Transactions of the Asme. 132. DOI: 10.1115/1.4002198 |
0.801 |
|
2010 |
Cardwell ND, Vlachos PP, Thole KA. A method for identifying and visualizing foreign particle motion using time-resolved particle tracking velocimetry Journal of Turbomachinery. 133. DOI: 10.1115/1.4001187 |
0.789 |
|
2010 |
Land CC, Joe C, Thole KA. Considerations of a double-wall cooling design to reduce sand blockage Journal of Turbomachinery. 132. DOI: 10.1115/1.3153308 |
0.491 |
|
2010 |
Ostanek JK, Prausa J, Van Suetendael A, Thole KA. Establishing a methodology for resolving convective heat transfer from complex geometries Journal of Turbomachinery. 132. DOI: 10.1115/1.3144989 |
0.515 |
|
2009 |
Cardwell ND, Vlachos PP, Thole KA. A method for identifying and visualizing foreign particle motion using time resolved particle tracking velocimetry Proceedings of the Asme Turbo Expo. 3: 979-990. DOI: 10.1115/GT2009-60273 |
0.786 |
|
2009 |
Lynch SP, Sundaram N, Thole KA, Kohli A, Lehane C. Heat transfer for a turbine blade with non-axisymmetric endwall contouring Proceedings of the Asme Turbo Expo. 3: 887-898. DOI: 10.1115/GT2009-60185 |
0.461 |
|
2009 |
Knost DG, Thole KA, Duggleby A. Evaluating a three-dimensional slot design for the combustor-turbine interface Proceedings of the Asme Turbo Expo. 3: 873-885. DOI: 10.1115/GT2009-60168 |
0.407 |
|
2009 |
Lawson SA, Thole KA. The effects of simulated particle deposition on film cooling Proceedings of the Asme Turbo Expo. 3: 41-51. DOI: 10.1115/GT2009-59109 |
0.365 |
|
2009 |
Cardwell ND, Vlachos PP, Thole KA. Developing and fully developed turbulent flow in ribbed channels 2008 Proceedings of the Asme Fluids Engineering Division Summer Conference, Fedsm 2008. 1: 379-388. DOI: 10.1115/FEDSM2008-55190 |
0.808 |
|
2009 |
Nasir S, Carullo JS, Ng WF, Thole KA, Wu H, Zhang LJ, Moon HK. Effects of large scale high freestream turbulence and exit reynolds number on turbine vane heat transfer in a transonic cascade Journal of Turbomachinery. 131. DOI: 10.1115/1.2952381 |
0.537 |
|
2009 |
Barringer MD, Thole KA, Polanka MD, Clark JP, Koch PJ. Migration of combustor exit profiles through high pressure turbine vanes Journal of Turbomachinery. 131. DOI: 10.1115/1.2950076 |
0.708 |
|
2009 |
Barringer MD, Thole KA, Polanka MD. An experimental study of combustor exit profile shapes on endwall heat transfer in high pressure turbine vanes Journal of Turbomachinery. 131. DOI: 10.1115/1.2950072 |
0.702 |
|
2009 |
Barringer MD, Thole KA, Polanka MD. Effects of combustor exit profiles on vane aerodynamic loading and heat transfer in a high pressure turbine Journal of Turbomachinery. 131. DOI: 10.1115/1.2950051 |
0.735 |
|
2008 |
Nasir S, Carullo JS, Ng WF, Thole KA, Wu H, Zhang LJ, Moon HK. Effects of large scale high freestream turbulence, and exit reynolds number on turbine vane heat transfer in a transonic cascade Asme International Mechanical Engineering Congress and Exposition, Proceedings. 8: 751-764. DOI: 10.1115/IMECE2007-44098 |
0.445 |
|
2008 |
Cardwell ND, Thole KA, Burd SW. Investigation of sand blocking within impingement and film-cooling holes Proceedings of the Asme Turbo Expo. 4: 1147-1159. DOI: 10.1115/1.3106702 |
0.837 |
|
2008 |
Sundaram N, Thole KA. Film-cooling flowfields with trenched holes on an endwall Proceedings of the Asme Turbo Expo. 4: 121-132. DOI: 10.1115/1.3068316 |
0.767 |
|
2008 |
Lynch SP, Thole KA. The effect of combustor-turbine interface gap leakage on the endwall heat transfer for a nozzle guide vane Journal of Turbomachinery. 130. DOI: 10.1115/1.2812950 |
0.776 |
|
2008 |
Sundaram N, Thole KA. Bump and trench modifications to film-cooling holes at the vane-endwall junction Journal of Turbomachinery. 130. DOI: 10.1115/1.2812933 |
0.772 |
|
2008 |
Colban W, Thole KA, Haendler M. A comparison of cylindrical and fan-shaped film-cooling holes on a vane endwall at low and high freestream turbulence levels Journal of Turbomachinery. 130. DOI: 10.1115/1.2720493 |
0.512 |
|
2008 |
Lawson MJ, Thole KA. Heat transfer augmentation along the tube wall of a louvered fin heat exchanger using practical delta winglets International Journal of Heat and Mass Transfer. 51: 2346-2360. DOI: 10.1016/J.Ijheatmasstransfer.2007.08.016 |
0.474 |
|
2007 |
Carullo JS, Nasir S, Cress RD, Ng WF, Thole KA, Zhang LJ, Moon HK. The effects of freestream turbulence, turbulence length scale and exit Reynolds number on turbine blade heat transfer in a transonic cascade Proceedings of the Asme Turbo Expo. 4: 1077-1089. DOI: 10.1115/GT2007-27859 |
0.478 |
|
2007 |
Lyall ME, Thrift AA, Kohli A, Thole KA. Heat transfer from low aspect ratio pin fins Proceedings of the Asme Turbo Expo. 4: 413-422. DOI: 10.1115/GT2007-27431 |
0.454 |
|
2007 |
Sundaram N, Thole KA. Bump and trench modifications to film-cooling holes at the vane endwall junction Proceedings of the Asme Turbo Expo. 4: 197-207. DOI: 10.1115/GT2007-27132 |
0.412 |
|
2007 |
Sundaram N, Barringer MD, Thole KA. Effects of deposits on film cooling of a vane endwall along the pressure side Proceedings of the Asme Turbo Expo. 4: 185-195. DOI: 10.1115/1.2812332 |
0.763 |
|
2007 |
Cardwell ND, Sundaram N, Thole KA. The effects of varying the combustor-turbine gap Journal of Turbomachinery. 129: 756-764. DOI: 10.1115/1.2720497 |
0.814 |
|
2007 |
Scrittore JJ, Thole KA, Burd SW. Investigation of velocity profiles for effusion cooling of a combustor liner Journal of Turbomachinery. 129: 518-526. DOI: 10.1115/1.2720492 |
0.541 |
|
2007 |
Sundaram N, Thole KA. Effects of surface deposition, hole blockage, and thermal barrier coating spallation on vane endwall film cooling Journal of Turbomachinery. 129: 599-607. DOI: 10.1115/1.2720485 |
0.769 |
|
2007 |
Barringer MD, Thole KA, Polanka MD. Experimental evaluation of an inlet profile generator for high-pressure turbine tests Journal of Turbomachinery. 129: 382-394. DOI: 10.1115/1.2436897 |
0.712 |
|
2007 |
Colban W, Thole KA, Haendler M. Experimental and computational comparisons of fan-shaped film cooling on a turbine vane surface Journal of Turbomachinery. 129: 23-31. DOI: 10.1115/1.2370747 |
0.544 |
|
2007 |
Colban W, Thole K. Influence of hole shape on the performance of a turbine vane endwall film-cooling scheme International Journal of Heat and Fluid Flow. 28: 341-356. DOI: 10.1016/J.Ijheatfluidflow.2006.05.002 |
0.507 |
|
2006 |
Bogard DG, Thole KA. Gas turbine film cooling Journal of Propulsion and Power. 22: 249-270. DOI: 10.2514/1.18034 |
0.773 |
|
2006 |
Lawson MJ, Sanders P, Thole KA. Computational and experimental comparison of tube wall heat transfer augmented by winglets in louvered fin heat exchangers American Society of Mechanical Engineers, Heat Transfer Division, (Publication) Htd. DOI: 10.1115/IMECE2006-14452 |
0.399 |
|
2006 |
Sundaram N, Thole KA. Effects of surface deposition, hole blockage, and TBC spallation on vane endwall film-cooling Proceedings of the Asme Turbo Expo. 3: 407-418. DOI: 10.1115/GT2006-90379 |
0.405 |
|
2006 |
Barringer MD, Thole KA, Polanka MD. Effects of combustor exit profiles on high pressure turbine vane aerodynamics and heat transfer Proceedings of the Asme Turbo Expo. 3: 285-295. DOI: 10.1115/GT2006-90277 |
0.687 |
|
2006 |
Kunze VR, Wolff M, Barringer MD, Thole KA, Polanka MD. Numerical insight into flow and thermal patterns within an inlet profile generator comparing to experimental results Proceedings of the Asme Turbo Expo. 3: 271-283. DOI: 10.1115/GT2006-90276 |
0.66 |
|
2006 |
Walsh WS, Thole KA, Joe C. Effects of sand ingestion on the blockage of film-cooling holes Proceedings of the Asme Turbo Expo. 3: 81-90. DOI: 10.1115/GT2006-90067 |
0.407 |
|
2006 |
Barringer MD, Thole KA, Polanka MD. Experimental evaluation of an inlet profile generator for high pressure turbine tests Proceedings of the Asme Turbo Expo. 3: 447-458. DOI: 10.1115/1.2436897 |
0.736 |
|
2006 |
Cardwell ND, Sundaram N, Thole KA. Effect of midpassage gap, endwall misalignment, and roughness on endwall film-cooling Journal of Turbomachinery. 128: 62-70. DOI: 10.1115/1.2098791 |
0.833 |
|
2006 |
Colban W, Gratton A, Thole KA, Haendler M. Heat transfer and film-cooling measurements on a stator vane with fan-shaped cooling holes Journal of Turbomachinery. 128: 53-61. DOI: 10.1115/1.2098789 |
0.582 |
|
2006 |
Sanders PA, Thole KA. Effects of winglets to augment tube wall heat transfer in louvered fin heat exchangers International Journal of Heat and Mass Transfer. 49: 4058-4069. DOI: 10.1016/J.Ijheatmasstransfer.2006.03.036 |
0.471 |
|
2006 |
Sewall EA, Tafti DK, Graham AB, Thole KA. Experimental validation of large eddy simulations of flow and heat transfer in a stationary ribbed duct International Journal of Heat and Fluid Flow. 27: 243-258. DOI: 10.1016/J.Ijheatfluidflow.2005.08.010 |
0.827 |
|
2006 |
Hada S, Thole KA. Study of leakage flows for a first vane in a gas turbine Proceedings of the 11th International Symposium On Transport Phenomena and Dynamics of Rotating Machinery, Isromac-11. 1: 330-343. |
0.518 |
|
2005 |
Couch E, Christophel J, Hohlfeld E, Thole KA, Cunha FJ. Comparison of measurements and predictions for blowing from a turbine blade tip Journal of Propulsion and Power. 21: 335-343. DOI: 10.2514/1.7238 |
0.516 |
|
2005 |
Hohlfeld EM, Christophel JR, Couch EL, Thole KA. Predictions of cooling from dirt purge holes along the tip of a turbine blade International Journal of Turbo and Jet Engines. 22: 139-152. DOI: 10.1515/Tjj.2005.22.3.139 |
0.558 |
|
2005 |
Knost DG, Thole KA. Computational predictions of endwall film-cooling for a first stage vane International Journal of Turbo and Jet Engines. 22: 41-58. DOI: 10.1515/Tjj.2005.22.1.41 |
0.522 |
|
2005 |
Colban W, Thole KA, Haendler M. Experimental and computational comparisons of fan-shaped film-cooling on a turbine vane surface American Society of Mechanical Engineers, Heat Transfer Division, (Publication) Htd. 376: 455-465. DOI: 10.1115/IMECE2005-79596 |
0.455 |
|
2005 |
Cardwell ND, Sundaram N, Thole KA. Effects of mid-passage gap, endwall misalignment and roughness on endwall film-cooling Proceedings of the Asme Turbo Expo. 3: 773-783. DOI: 10.1115/GT2005-68900 |
0.845 |
|
2005 |
Scrittore JJ, Thole KA, Burd SW. Experimental characterization of film-cooling effectiveness near combustor dilution holes Proceedings of the Asme Turbo Expo. 3: 1339-1347. DOI: 10.1115/GT2005-68704 |
0.461 |
|
2005 |
Kunze VR, Wolff M, Barringer MD, Thole KA, Polanka MD. Numerical modeling of flow and thermal patterns within a combustor simulator Proceedings of the Asme Turbo Expo. 6: 519-528. DOI: 10.1115/GT2005-68284 |
0.702 |
|
2005 |
Ranson WW, Thole KA, Cunha FJ. Adiabatic effectiveness measurements and predictions of leakage flows along a blade endwall Journal of Turbomachinery. 127: 609-618. DOI: 10.1115/1.1929809 |
0.51 |
|
2005 |
Christophel JR, Thole KA, Cunha FJ. Cooling the tip of a turbine blade using pressure side holes - Part I: Adiabatic effectiveness measurements Journal of Turbomachinery. 127: 270-277. DOI: 10.1115/1.1812320 |
0.525 |
|
2005 |
Knost DG, Thole KA. Adiabatic effectiveness measurements of endwall film-cooling for a first-stage vane Journal of Turbomachinery. 127: 297-305. DOI: 10.1115/1.1811099 |
0.547 |
|
2005 |
Christophel JR, Thole KA, Cunha FJ. Cooling the tip of a turbine blade using pressure side holes - Part II: Heat transfer measurements Journal of Turbomachinery. 127: 278-286. DOI: 10.1115/1.1811096 |
0.584 |
|
2005 |
Christophel JR, Couch E, Thole KA, Cunha FJ. Measured adiabatic effectiveness and heat transfer for blowing from the tip of a turbine blade Journal of Turbomachinery. 127: 251-262. DOI: 10.1115/1.1811095 |
0.568 |
|
2005 |
Vakil SS, Thole KA. Flow and thermal field measurements in a combustor simulator relevant to a gas turbine aeroengine Journal of Engineering For Gas Turbines and Power. 127: 257-267. DOI: 10.1115/1.1806455 |
0.442 |
|
2005 |
Thole KA, Knost DG. Heat transfer and film-cooling for the endwall of a first stage turbine vane International Journal of Heat and Mass Transfer. 48: 5255-5269. DOI: 10.1016/J.Ijheatmasstransfer.2005.07.036 |
0.588 |
|
2005 |
Stephan RA, Thole KA. Optimization study relevant to louvered fin compact heat exchangers International Journal of Heat Exchangers. 6: 73-92. |
0.341 |
|
2004 |
Lethander AT, Thole KA, Zess G, Wagner J. Vane-endwall junction optimization to reduce turbine vane passage adiabatic wall temperatures Journal of Propulsion and Power. 20: 1105-1116. DOI: 10.2514/1.3887 |
0.465 |
|
2004 |
Stitzel S, Thole KA. Flow field computations of combustor-turbine interactions relevant to a gas turbine engine Journal of Turbomachinery. 126: 122-129. DOI: 10.1115/1.1625691 |
0.472 |
|
2004 |
Knost DG, Thole KA. Adiabatic effectiveness measurements of endwall film-cooling for a first stage vane Proceedings of the Asme Turbo Expo 2004. 3: 353-362. |
0.456 |
|
2004 |
Graham A, Sewall E, Thole KA. Flowfield measurements in a ribbed channel relevant to internal turbine blade cooling Proceedings of the Asme Turbo Expo 2004. 3: 383-391. |
0.354 |
|
2004 |
Barringer MD, Thole KA, Polanka MD. Developing a combustor simulator for investigating high pressure turbine aerodynamics and heat transfer Proceedings of the Asme Turbo Expo 2004. 3: 565-575. |
0.702 |
|
2004 |
Christophel JR, Thole KA, Cunha FJ. Cooling the tip of a turbine blade using pressure side holes - Part 1: Adiabatic effectiveness measurements Proceedings of the Asme Turbo Expo 2004. 3: 263-271. |
0.418 |
|
2004 |
Christophel JR, Thole KA, Cunha FJ. Cooling the tip of a turbine blade using pressure side holes - Part 2: Heat transfer measurements Proceedings of the Asme Turbo Expo 2004. 3: 273-282. |
0.472 |
|
2004 |
Ebeling CP, Thole KA. Measurements and predictions of the heat transfer at the tube-fin junction for louvered fin heat exchangers International Journal of Heat Exchangers. 5: 265-286. |
0.385 |
|
2003 |
Lethander AT, Thole KA, Zess G, Wagner J. Optimizing the vane-endwall junction to reduce adiabatic wall temperatures in a turbine vane passage American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) Igti. 5: 711-721. DOI: 10.1115/GT2003-38939 |
0.356 |
|
2003 |
Vakil SS, Thole KA. Flow and thermal field measurements in a combustor simulator relevant to a gas turbine aero-engine American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) Igti. 2: 215-224. DOI: 10.1115/GT2003-38254 |
0.337 |
|
2003 |
Colban WF, Lethander AT, Thole KA, Zess G. Combustor turbine interface studies - Part 2: Flow and thermal field measurements Journal of Turbomachinery. 125: 203-209. DOI: 10.1115/1.1561812 |
0.499 |
|
2003 |
Colban WF, Thole KA, Zess G. Combustor turbine interface studies - Part 1: Endwall effectiveness measurements Journal of Turbomachinery. 125: 193-202. DOI: 10.1115/1.1561811 |
0.538 |
|
2002 |
Nix AC, Smith AC, Diller TE, Ng WF, Thole KA. High intensity, large length-scale freestream turbulence generation in a transonic turbine cascade American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) Igti. 3: 961-968. DOI: 10.1115/GT2002-30523 |
0.408 |
|
2002 |
Hermanson KS, Thole KA. Effect of non-uniform inlet conditions on endwall secondary flows American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) Igti. 3: 245-254. DOI: 10.1115/1.1505849 |
0.476 |
|
2002 |
Hermanson KS, Thole KA. Effect of nonuniform inlet conditions on endwall secondary flows Journal of Turbomachinery. 124: 623-631. DOI: 10.1115/1.1505849 |
0.392 |
|
2002 |
Barringer MD, Richard OT, Walter JP, Stitzel SM, Thole KA. Flow field simulations of a gas turbine combustor Journal of Turbomachinery. 124: 508-516. DOI: 10.1115/1.1475742 |
0.465 |
|
2002 |
Zess GA, Thole KA. Computational design and experimental evaluation of using a leading edge fillet on a gas turbine vane Journal of Turbomachinery. 124: 167-175. DOI: 10.1115/1.1460914 |
0.46 |
|
2002 |
Radomsky RW, Thole KA. Detailed boundary layer measurements on a turbine stator vane at elevated freestream turbulence levels Journal of Turbomachinery. 124: 107-118. DOI: 10.1115/1.1424891 |
0.415 |
|
2002 |
Lyman AC, Stephan RA, Thole KA, Zhang LW, Memory SB. Scaling of heat transfer coefficients along louvered fins Experimental Thermal and Fluid Science. 26: 547-563. DOI: 10.1016/S0894-1777(02)00163-2 |
0.496 |
|
2002 |
Thole KA, Radomsky RW, Kang MB, Kohli A. Elevated freestream turbulence effects on heat transfer for a gas turbine vane International Journal of Heat and Fluid Flow. 23: 137-147. DOI: 10.1016/S0142-727X(01)00145-X |
0.832 |
|
2001 |
Harrington MK, McWaters MA, Bogard DG, Lemmon CA, Thole KA. Full-coverage film cooling with short normal injection holes Journal of Turbomachinery. 123: 798-805. DOI: 10.1115/1.1400111 |
0.77 |
|
2000 |
Hermanson KS, Thole KA. Effect of inlet conditions on endwall secondary flows Journal of Propulsion and Power. 16: 286-296. DOI: 10.2514/2.5567 |
0.502 |
|
2000 |
Hermanson KS, Thole KA. Effect of Mach number on secondary flow characteristics International Journal of Turbo and Jet Engines. 17: 179-196. DOI: 10.1515/Tjj.2000.17.3.179 |
0.515 |
|
2000 |
Radomsky RW, Thole KA. High freestream turbulence effects on endwall heat transfer for a gas turbine stator vane Proceedings of the Asme Turbo Expo. 3. DOI: 10.1115/2000-GT-0201 |
0.474 |
|
2000 |
Radomsky RW, Thole KA. Flowfield measurements for a highly turbulent flow in a stator vane passage Journal of Turbomachinery. 122: 255-262. DOI: 10.1115/1.555442 |
0.53 |
|
2000 |
Radomsky RW, Thole KA. Measurements and predictions of a highly turbulent flowfield in a turbine vane passage Journal of Fluids Engineering, Transactions of the Asme. 122: 666-676. DOI: 10.1115/1.1313244 |
0.434 |
|
2000 |
Radomsky RW, Thole KA. High free-steam turbulence effects on endwall heat transfer for a gas turbine stator vane Journal of Turbomachinery. 122: 699-708. DOI: 10.1115/1.1312807 |
0.548 |
|
2000 |
Kang MB, Thole KA. Flowfield measurements in the endwall region of a stator vane Journal of Turbomachinery. 122: 458-466. DOI: 10.1115/1.1303703 |
0.539 |
|
1999 |
Kang MB, Kohli A, Thole KA. Closure to “Discussion of ‘Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall’” (1999, ASME J. Turbomach., 121, p. 568) Journal of Turbomachinery-Transactions of the Asme. 121: 568-568. DOI: 10.1115/1.2841353 |
0.326 |
|
1999 |
Kang MB, Kohli A, Thole KA. Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall Journal of Turbomachinery-Transactions of the Asme. 121: 558-568. DOI: 10.1115/1.2841351 |
0.54 |
|
1999 |
Springer ME, Thole KA. Entry region of louvered fin heat exchangers Experimental Thermal and Fluid Science. 19: 223-232. DOI: 10.1016/S0894-1777(99)00028-X |
0.506 |
|
1998 |
Thole KA, Gritsch M, Schulz A, Wittig S. Flowfield Measurements for Film-Cooling Holes With Expanded Exits Journal of Turbomachinery-Transactions of the Asme. 120: 327-336. DOI: 10.1115/1.2841410 |
0.457 |
|
1998 |
Springer ME, Thole KA. Experimental design for flowfield studies of louvered fins Experimental Thermal and Fluid Science. 18: 258-269. DOI: 10.1016/S0894-1777(98)10022-5 |
0.492 |
|
1997 |
Thole KA, Gritsch M, Schulz A, Wittig S. Effect of a Crossflow at the Entrance to a Film-Cooling Hole Journal of Fluids Engineering-Transactions of the Asme. 119: 533-540. DOI: 10.1115/1.2819277 |
0.487 |
|
1996 |
Thole KA, Bogard DG. High Freestream Turbulence Effects on Turbulent Boundary Layers Journal of Fluids Engineering-Transactions of the Asme. 118: 276-284. DOI: 10.1115/1.2817374 |
0.719 |
|
1995 |
Laudon MF, Thole KA, Engelstad RL, Resnick DJ, Cummings KD, Dauksher WJ. Thermal analysis of an x‐ray mask membrane in a plasma environment Journal of Vacuum Science & Technology B. 13: 3050-3054. DOI: 10.1116/1.588320 |
0.355 |
|
1995 |
Thole KA, Bogard DG. Enhanced Heat Transfer and Shear Stress Due to High Free-Stream Turbulence Journal of Turbomachinery-Transactions of the Asme. 117: 418-424. DOI: 10.1115/1.2835677 |
0.76 |
|
1994 |
Thole KA, Bogard DG. Simultaneous temperature and velocity measurements Measurement Science and Technology. 5: 435-439. DOI: 10.1088/0957-0233/5/4/018 |
0.709 |
|
1994 |
Thole KA, Bogard DG, Whan-Tong JL. Generating high freestream turbulence levels Experiments in Fluids. 17: 375-380. DOI: 10.1007/Bf01877037 |
0.742 |
|
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