| Design and evaluation of an additively manufactured aircraft heat exchanger D Saltzman, M Bichnevicius, S Lynch, TW Simpson, EW Reutzel, ... Applied Thermal Engineering 138, 254-263, 2018 | 142 | 2018 |
| Heat transfer for a turbine blade with nonaxisymmetric endwall contouring SP Lynch, N Sundaram, KA Thole, A Kohli, C Lehane | 109 | 2011 |
| The effect of combustor-turbine interface gap leakage on the endwall heat transfer for a nozzle guide vane SP Lynch, KA Thole | 79 | 2008 |
| Genetic algorithm based topology optimization of heat exchanger fins used in aerospace applications BS Mekki, J Langer, S Lynch International Journal of Heat and Mass Transfer 170, 121002, 2021 | 78 | 2021 |
| Computational predictions of heat transfer and film-cooling for a turbine blade with nonaxisymmetric endwall contouring SP Lynch, KA Thole, A Kohli, C Lehane | 71 | 2011 |
| The effect of the combustor-turbine slot and midpassage gap on vane endwall heat transfer SP Lynch, KA Thole | 63 | 2011 |
| The effect of area ratio change via increased hole length for shaped film cooling holes with constant expansion angles S Haydt, S Lynch, S Lewis Journal of Turbomachinery 140 (5), 051002, 2018 | 39 | 2018 |
| The effect of combustor-turbine interface gap leakage on the endwall heat transfer for a nozzle guide vane SP Lynch, KA Thole Turbo Expo: Power for Land, Sea, and Air 47934, 671-682, 2007 | 32 | 2007 |
| Cooling effectiveness for a shaped film cooling hole at a range of compound angles S Haydt, S Lynch Journal of Turbomachinery 141 (4), 041005, 2019 | 31 | 2019 |
| The Effect of a Meter-Diffuser Offset on Shaped Film Cooling Hole Adiabatic Effectiveness S Haydt, S Lynch, S Lewis Journal of Turbomachinery 139 (9), 091012, 2017 | 31 | 2017 |
| Comparison of the three-dimensional boundary layer on flat versus contoured turbine endwalls SP Lynch, KA Thole Journal of Turbomachinery 138 (4), 041008, 2016 | 29 | 2016 |
| Time-resolved stereo PIV measurements of the horseshoe vortex system at multiple locations in a low-aspect-ratio pin–fin array CD Anderson, SP Lynch Experiments in Fluids 57, 1-18, 2016 | 29 | 2016 |
| Heat transfer and film cooling on a contoured blade endwall with platform gap leakage SP Lynch, KA Thole Journal of Turbomachinery 139 (5), 051002, 2017 | 27 | 2017 |
| Experimental comparison of a traditionally built versus additively manufactured aircraft heat exchanger DJ Saltzman, M Bichnevicius, SP Lynch, T Simpson, T Reutzel, ... 55th AIAA Aerospace Sciences Meeting, 0902, 2017 | 26 | 2017 |
| Review of advances in convective heat transfer developed through additive manufacturing KA Thole, SP Lynch, AJ Wildgoose Advances in Heat Transfer 53, 249-325, 2021 | 23 | 2021 |
| Simulations of multiphase particle deposition on a nonaxisymmetric contoured endwall with film-cooling SA Lawson, SP Lynch, KA Thole Journal of turbomachinery 135 (3), 031032, 2013 | 22 | 2013 |
| Effect of Reynolds number on turbulent junction flow fluid dynamics and heat transfer SS Elahi, EA Lange, SP Lynch International Journal of Heat and Mass Transfer 142, 118328, 2019 | 18 | 2019 |
| Experimental heat transfer and boundary layer measurements on a ceramic matrix composite surface PH Wilkins, SP Lynch, KA Thole, S Quach, T Vincent Journal of Turbomachinery 143 (6), 061010, 2021 | 17 | 2021 |
| Time-resolved PIV measurements of the effect of freestream turbulence on horseshoe vortex dynamics E Lange, SS Elahi, S Lynch 2018 AIAA Aerospace Sciences Meeting, 0584, 2018 | 16 | 2018 |
| Comparison of additively manufactured louvered plate-fin heat exchangers M Bichnevicius, D Saltzman, S Lynch Journal of Thermal Science and Engineering Applications 12 (1), 011018, 2020 | 15 | 2020 |
