| Chevron film cooled wall CP Lee, SR Brassfield, RS Bunker US Patent 7,328,580, 2008 | 347 | 2008 |
| Method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture RS Bunker, JC Bailey, CP Lee, N Abuaf US Patent 6,234,755, 2001 | 202 | 2001 |
| Heat transfer coefficients on the squealer tip and near-tip regions of a gas turbine blade with single or double squealer JS Kwak, J Ahn, JC Han, CP Lee, RS Bunker, R Boyle, R Gaugler J. Turbomach. 125 (4), 778-787, 2003 | 170 | 2003 |
| Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part II—Effect on Film Effectiveness and Heat Transfer Distributions AB Mehendale, JC Han, S Ou, CP Lee | 157 | 1994 |
| Effect of squealer geometry arrangement on a gas turbine blade tip heat transfer GS Azad, JC Han, RS Bunker, CP Lee J. Heat Transfer 124 (3), 452-459, 2002 | 146 | 2002 |
| Effects of surface roughness on heat transfer and aerodynamic performance of turbine airfoils N Abuaf, RS Bunker, CP Lee | 132 | 1998 |
| Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part I—Effect on Heat Transfer Coefficients S Ou, JC Han, AB Mehendale, CP Lee | 123 | 1994 |
| Air-cooled turbine blade RJ Corsmeier, HM Maclin, CP Lee US Patent 5,813,835, 1998 | 120 | 1998 |
| Turbine blade squealer tip peripheral end wall with cooling passage arrangement CP Lee US Patent 5,660,523, 1997 | 120 | 1997 |
| Scaled heat transfer surface with protruding ramp surface turbulators CP Lee, JW Savage, M Bobo US Patent 5,361,828, 1994 | 118 | 1994 |
| Scalloped surface turbine stage A Tam, CP Lee, KR Kirtley, RS Bunker, SH Lamson, SM Carson US Patent 7,134,842, 2006 | 114 | 2006 |
| Modulated turbine cooling system GA Durgin, RC Bauer, CP Lee US Patent 6,050,079, 2000 | 112 | 2000 |
| Augmented heat transfer in square channels with wedge-shaped and delta-shaped turbulence promoters JC Han, JJ Huang, CP Lee Journal of Enhanced Heat Transfer 1 (1), 1994 | 112 | 1994 |
| Film cooled wall CP Lee US Patent 5,419,681, 1995 | 105 | 1995 |
| Analysis of some improved blade tip concepts C Prakash, CP Lee, DG Cherry, R Doughty, AR Wadia | 103 | 2006 |
| Twin rib turbine blade CP Lee US Patent 6,059,530, 2000 | 102 | 2000 |
| Airfoil cooling circuits and method SR Brassfield, CP Lee, RL Doughty, RW Jendrix, CM Williams US Patent 7,377,746, 2008 | 100 | 2008 |
| Crescentic ramp turbine stage CP Lee, A Tam, KR Kirtley, SH Lamson US Patent 7,220,100, 2007 | 100 | 2007 |
| Turbulator configuration for cooling passages of an airfoil in a gas turbine engine CP Lee, DB Knable US Patent 5,738,493, 1998 | 98 | 1998 |
| Directly cooled thermal barrier coating system CP Lee, RE Schafrik, R Darolia US Patent 6,617,003, 2003 | 97 | 2003 |
