| Performance-analysis-based gas turbine diagnostics: A review YG Li Proceedings of the Institution of Mechanical Engineers, Part A: Journal of …, 2002 | 361 | 2002 |
| Gas turbine performance prognostic for condition-based maintenance YG Li, P Nilkitsaranont Applied energy 86 (10), 2152-2161, 2009 | 318 | 2009 |
| Review of Modern Lower Emissions Combustion Technology for Aero Gas Turbine Engines NDLYG Liu Y., Sun X., Sethi V., Wang L. Progress in Aerospace Sciences 94, 12-45, 2017 | 291* | 2017 |
| Gas Turbine Performance and Health Status Estimation Using Adaptive Gas Path Analysis L Y.G. ASME Turbo Expo 2009, GT2009-59168, 2009 | 142 | 2009 |
| Non-Linear Multiple Gas Turbine Off-Design Performance Adaptation Using a Genetic Algorithm L Y.G., AG M.F., W L., S R., H K., F X. ASME Turbo Expo 2010, GT2010-22285,, 2010 | 93* | 2010 |
| Multiple-point adaptive performance simulation tuned to aeroengine test-bed data YG Li, L Marinai, EL Gatto, V Pachidis, P Philidis Journal of Propulsion and Power 25 (3), 635-641, 2009 | 93 | 2009 |
| An Adaptation Approach for Gas Turbine Design-Point Performance Simulation L Y.G., P P., N M. ASME TURBO EXPO 2005, GT2005-68140, 2005 | 90 | 2005 |
| An advanced gas turbine gas path diagnostic system-PYTHIA YG Li, R Singh XVII International Symposium on Air Breathing Engines, Munich, Germany …, 2005 | 80 | 2005 |
| Gas path fault diagnosis of a turbofan engine from transient data using artificial neural networks SOT Ogaji, YG Li, S Sampath, R Singh Turbo Expo: Power for Land, Sea, and Air 36843, 405-414, 2003 | 73 | 2003 |
| Improved Multiple Point Non-Linear Genetic Algorithm Based Performance Adaptation Using Least Square Method L Y.G., AG M.F., W L., S R., H K., F X., Z W. ASME Turbo Expo 2011, GT2011-45289, 2011 | 65 | 2011 |
| GA-based design-point performance adaptation and its comparison with ICM-based approach YG Li, P Pilidis Applied Energy 87 (1), 340-348, 2010 | 59 | 2010 |
| A gas turbine diagnostic approach with transient measurements YG Li Proceedings of the Institution of Mechanical Engineers, Part A: Journal of …, 2003 | 59 | 2003 |
| Transient performance simulation of aircraft engine integrated with fuel and control systems C Wang, YG Li, BY Yang Applied Thermal Engineering 114, 1029-1037, 2017 | 56 | 2017 |
| Performance-based fault diagnosis of a gas turbine engine using an integrated support vector machine and artificial neural network method AD Fentaye, SI Ul-Haq Gilani, AT Baheta, YG Li Proceedings of the Institution of Mechanical Engineers, Part A: Journal of …, 2019 | 55 | 2019 |
| Gas turbine off-design performance adaptation using a genetic algorithm E Lo Gatto, YG Li, P Pilidis Turbo Expo: Power for Land, Sea, and Air 42371, 551-560, 2006 | 44 | 2006 |
| Effect of fouling, thermal barrier coating degradation and film cooling holes blockage on gas turbine engine creep life EA Ogiriki, YG Li, T Nikolaidis, TGE Isaiah, G Sule Procedia Cirp 38, 228-233, 2015 | 43 | 2015 |
| Measurement Selection for Multi-Component Gas Path Diagnostics Using Analytical Approach and Measurement Subset Concept J M.S., L Y.G. ASME Turbo Expo 2010, GT2010-22402, 2010 | 42* | 2010 |
| Nonlinear weighted-least-squares estimation approach for gas-turbine diagnostic applications YG Li, T Korakiantis Journal of Propulsion and Power 27 (2), 337-345, 2011 | 38 | 2011 |
| Fault diagnosis of a two spool turbo-fan engine using transient data: A genetic algorithm approach S Sampath, YG Li, SOT Ogaji, R Singh Turbo Expo: Power for Land, Sea, and Air 36843, 351-359, 2003 | 37 | 2003 |
| Aero Gas Turbine Flight Performance Estimation Using Engine Gas Path Measurements L Y.G. 21st ISABE Conference, ISABE-2013-1729, 2013 | 36 | 2013 |
