| Thermal cycle analysis of turboelectric distributed propulsion system with boundary layer ingestion C Liu, G Doulgeris, P Laskaridis, R Singh Aerospace Science and Technology 27 (1), 163-170, 2013 | 50 | 2013 |
| An integrated engine-aircraft performance platform for assessing new technologies in aeronautics P Laskaridis, P Pilidis, P Kotsiopoulos International Society for air-Breathing engines conference, 1-13, 2005 | 50 | 2005 |
| Industrial gas turbine performance: compressor fouling and on-line washing U Igie, P Pilidis, D Fouflias, K Ramsden, P Laskaridis Journal of turbomachinery 136 (10), 101001, 2014 | 49 | 2014 |
| Performance investigations and systems architectures for the more electric aircraft P Laskaridis Cranfield University, 2004 | 48 | 2004 |
| Aero-engine turbine blade life assessment using the Neu/Sehitoglu damage model AO Abu, S Eshati, P Laskaridis, R Singh International Journal of Fatigue 61, 160-169, 2014 | 46 | 2014 |
| An assessment of distributed propulsion: Advanced propulsion system architectures for conventional aircraft configurations R Kirner, L Raffaelli, A Rolt, P Laskaridis, G Doulgeris, R Singh Aerospace Science and Technology 46, 42-50, 2015 | 44 | 2015 |
| Assessment of numerical radiation models on the heat transfer of an aero-engine combustion chamber AAA Gamil, T Nikolaidis, I Lelaj, P Laskaridis Case Studies in Thermal Engineering 22, 100772, 2020 | 36 | 2020 |
| Methodology to assess the performance of an aircraft concept with distributed propulsion and boundary layer ingestion using a parametric approach EA Valencia, D Nalianda, P Laskaridis, R Singh Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2015 | 36 | 2015 |
| An assessment of distributed propulsion: Part B–Advanced propulsion system architectures for blended wing body aircraft configurations R Kirner, L Raffaelli, A Rolt, P Laskaridis, G Doulgeris, R Singh Aerospace Science and Technology 50, 212-219, 2016 | 35 | 2016 |
| Influence of water–air ratio on the heat transfer and creep life of a high pressure gas turbine blade S Eshati, A Abu, P Laskaridis, F Khan Applied Thermal Engineering 60 (1-2), 335-347, 2013 | 35 | 2013 |
| Impact of operating conditions and design parameters on gas turbine hot section creep life S Eshati, MF Abdul Ghafir, P Laskaridis, YG Li Turbo Expo: Power for Land, Sea, and Air 43987, 547-558, 2010 | 29 | 2010 |
| Effects of off-takes for aircraft secondary-power systems on jet engine efficiency P Giannakakis, P Laskaridis, P Pilidis Journal of Propulsion and Power 27 (5), 1024-1031, 2011 | 27 | 2011 |
| Full-aircraft energy-based force decomposition applied to boundary-layer ingestion DS Sanders, P Laskaridis AIAA Journal 58 (10), 4357-4373, 2020 | 26 | 2020 |
| Performance characteristics and optimisation of a geared intercooled reversed flow core engine W Camilleri, E Anselmi, V Sethi, P Laskaridis, A Rolt, P Cobas Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2015 | 24 | 2015 |
| Severity estimation and effect of operational parameters for civil aircraft jet engines H Hanumanthan, A Stitt, P Laskaridis, R Singh Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2012 | 22 | 2012 |
| Transient modelling and simulation of gas turbine secondary air system T Nikolaidis, H Wang, P Laskaridis Applied thermal engineering 170, 115038, 2020 | 21 | 2020 |
| Discretized Miller approach to assess effects on boundary layer ingestion induced distortion E Valencia, V Hidalgo, D Nalianda, P Laskaridis, R Singh Chinese Journal of Aeronautics 30 (1), 235-248, 2017 | 21 | 2017 |
| Toward a scalable propeller performance map P Giannakakis, P Laskaridis, T Nikolaidis, AI Kalfas Journal of Propulsion and Power 31 (4), 1073-1082, 2015 | 20 | 2015 |
| Investigation into the effects of operating conditions and design parameters on the creep life of high pressure turbine blades in a stationary gas turbine engine HA Eshati Samir , Abu Abdulahi , Laskaridis Panagiotis Mechanics and Mechanical Engineering 5 (3), 237-247, 2011 | 20* | 2011 |
| Novel fan configuration for distributed propulsion systems with boundary layer ingestion on an hybrid wing body airframe E Valencia, V Alulema, D Rodriguez, P Laskaridis, I Roumeliotis Thermal Science and Engineering Progress 18, 100515, 2020 | 19 | 2020 |
