| The effects of combustor cooling features on nozzle guide vane film cooling experiments NE Holgate, PT Ireland, E Romero Journal of Turbomachinery 141 (1), 011005, 2019 | 10 | 2019 |
| Prediction and augmentation of nozzle guide vane film cooling hole pressure margin NE Holgate, I Cresci, PT Ireland, AJ Rawlinson 12 th European Conference on Turbomachinery Fluid dynamics & Thermodynamics, 2017 | 8 | 2017 |
| Efficient visibility criterion for discontinuities discretised by triangular surface meshes N Holgate, GR Joldes, K Miller Engineering analysis with boundary elements 58, 1-6, 2015 | 7 | 2015 |
| Nozzle Guide Vane Film Cooling Effectiveness for Radial Showerheads With Restricted Cooling Hole Surface Angles NE Holgate, PT Ireland, KP Self Turbo Expo: Power for Land, Sea, and Air 50893, V05CT19A023, 2017 | 5 | 2017 |
| An experimental-numerical method for transient infrared measurement of film cooling effectiveness and heat transfer coefficient in a single test NE Holgate, PT Ireland, E Romero The Aeronautical Journal 123 (1270), 1982-1998, 2019 | 4 | 2019 |
| Coolant Jets Blowing Across the Airfoil Stagnation Line to Enhance Film Effectiveness NE Holgate, PT Ireland, E Romero Journal of Turbomachinery 142 (6), 061005, 2020 | 1 | 2020 |
| Novel leading edge film cooling experiments and geometries NE Holgate University of Oxford (United Kingdom), 2019 | | 2019 |
Peter IrelandUniversity of OxfordE-mail megerősítve itt: eng.ox.ac.uk
