| Fan root aerodynamics for large bypass gas turbine engines: Influence on the engine performance and 3D design G Zamboni, L Xu Turbo Expo: Power for Land, Sea, and Air 48883, 167-178, 2009 | 210 | 2009 |
| Gradient-based adjoint and design of experiment CFD methodologies to improve the manufacturability of high pressure turbine blades G Zamboni, G Banks, S Bather Turbo Expo: Power for Land, Sea, and Air 49712, V02CT39A001, 2016 | 25 | 2016 |
| Fan root aerodynamics for large bypass gas turbine engines: Influence on the engine performance and 3D design G Zamboni, L Xu Journal of turbomachinery 134 (6), 2012 | 20 | 2012 |
| Normal-shock/boundary-layer interactions in transonic intakes at high incidence A Coschignano, H Babinsky, C Sheaf, G Zamboni AIAA Journal 57 (7), 2867-2880, 2019 | 13 | 2019 |
| On the unsteady interaction between the leakage and the main passage flow in a high pressure turbine rig: Cfd urans investigations and comparison with the rig test data G Zamboni, P Adami Turbo Expo: Power for Land, Sea, and Air 49705, V02BT38A002, 2016 | 11 | 2016 |
| A high fidelity quality assessment of high pressure turbine blades using surface curvature and gradient-based adjoint A Mulloth, G Banks, G Zamboni, S Bather Turbo Expo: Power for Land, Sea, and Air 51005, V02BT41A003, 2018 | 3 | 2018 |
| Method of manufacturing and inspecting gas washed components in a gas turbine engine S Bather, G Zamboni US Patent App. 15/611,162, 2017 | 2 | 2017 |
| Fan exhaust for a gas turbine engine MJ Wilson, G Zamboni US Patent App. 15/868,066, 2018 | 1 | 2018 |
| Fan root aerodynamics G Zamboni University of Cambridge, 2009 | 1 | 2009 |
| Method of manufacturing and inspecting gas washed components in a gas turbine engine S Bather, G Zamboni US Patent 10,663,275, 2020 | | 2020 |
| Compressor G Zamboni US Patent App. 12/222,837, 2009 | | 2009 |
