| Heat transfer by laminar flow from a rotating plate K Millsaps, K Pohlhausen Journal of the Aeronautical Sciences 19 (2), 120-126, 1952 | 340 | 1952 |
| Thermal distributions in Jeffery-Hamel flows between nonparallel plane walls K Millsaps, K Pohlhausen Journal of the Aeronautical Sciences 20 (3), 187-196, 1953 | 184 | 1953 |
| Effects of Reynolds number and surface roughness magnitude and location on compressor cascade performance SC Back, GV Hobson, SJ Song, KT Millsaps | 59 | 2012 |
| The laminar free-convective heat transfer from the outer surface of a vertical circular cylinder K MILLSAPS, K POHLHAUSEN Journal of the Aerospace Sciences 25 (6), 357-360, 1958 | 46 | 1958 |
| Reducing lateral vibrations of a rotor passing through critical speeds by acceleration scheduling KT Millsaps, GL Reed | 44 | 1998 |
| Detection and localization of fouling in a gas turbine compressor from aerothermodynamic measurements KT Millsaps, J Baker, JS Patterson Turbo Expo: Power for Land, Sea, and Air 41707, 1867-1876, 2004 | 33 | 2004 |
| Heat transfer to Hagen-Poiseuille flows K Millsaps, K Pohlhausen Proceedings of the Conference on Differential Equations, University of …, 1955 | 31 | 1955 |
| Impact of nonuniform leading edge coatings on the aerodynamic performance of compressor airfoils ME Elmstrom, KT Millsaps, GV Hobson, JS Patterson | 27 | 2011 |
| Constant acceleration of an undamped simple vibrator through resonance RL Fearn, K Millsaps The Aeronautical Journal 71 (680), 567-569, 1967 | 27 | 1967 |
| Integrated electric gas turbine KT Millsaps Jr US Patent 7,661,271, 2010 | 25 | 2010 |
| Combustion characterization and ignition delay modeling of low-and high-cetane alternative diesel fuels in a marine diesel engine J Petersen, D Seivwright, P Caton, K Millsaps Energy & Fuels 28 (8), 5463-5471, 2014 | 20 | 2014 |
| Effect of leading edge roughness and Reynolds number on compressor profile loss JH Im, JH Shin, GV Hobson, SJ Song, KT Millsaps Turbo Expo: Power for Land, Sea, and Air 55225, V06AT35A034, 2013 | 18 | 2013 |
| Dynamic Forces From Single Gland Labyrinth Seals: Part I—Ideal and Viscous Decomposition KT Millsaps, M Martinez-Sanchez | 18 | 1994 |
| The impact of unsteady swirling flow in a single gland labyrinth seal on rotordynamic stability: theory and experiment KT Millsaps Massachusetts Institute of Technology, 1992 | 17 | 1992 |
| Rotordynamic forces in labyrinth seals: Theory and experiment KT Millsaps, M Martinez-Sanchez NASA. Lewis Research Center, Rotordynamic Instability Problems in High …, 1994 | 16 | 1994 |
| Heat transfer in a laminar cyclone I K Millsaps, JE Nydahl ZAMM‐Journal of Applied Mathematics and Mechanics/Zeitschrift für Angewandte …, 1973 | 11 | 1973 |
| Application of the galerkin method to the prandtl lifting line equation RC ANDERSON, K MlLLSAPS Journal of Aircraft 1 (3), 126-128, 1964 | 11 | 1964 |
| Effect of surface roughness location and reynolds number on compressor cascade performance SC Back, GV Hobson, SJ Song, KT Millsaps Turbo Expo: Power for Land, Sea, and Air 44021, 121-128, 2010 | 10 | 2010 |
| Impact of Non-uniform leading edge coatings on the aerodynamic performance of compressor airfoils ME Elmstrom, KT Millsaps, GV Hobson, JS Patterson Turbo Expo: Power for Land, Sea, and Air 47306, 103-113, 2005 | 10 | 2005 |
| Dynamic Forces From Single Gland Labyrinth Seals: Part II—Upstream Coupling KT Millsaps, M Martinez-Sanchez | 10 | 1994 |
