| Taylor-Couette-Poiseuille flow heat transfer in a high Taylor number test rig PB Swann, H Russell, IH Jahn Journal of the Global Power and Propulsion Society 5, 126-147, 2021 | 18 | 2021 |
| Rotating shaft thermal analysis for supercritical carbon dioxide radial inflow turbines PB Swann, H Russell, I Jahn 15th International Energy Conversion Engineering Conference, 4864, 2017 | 14 | 2017 |
| Supercritical carbon dioxide Taylor–Couette–Poiseuille flow heat transfer P Swann, I Jahn, H Russell International Journal of Heat and Mass Transfer 183, 122204, 2022 | 13 | 2022 |
| Investigation into Taylor-Couette-Poiseuille flow heat transfer for supercritical carbon dioxide turbomachinery P Swann | 6 | 2020 |
| Reconfiguring the TUSQ Hypersonic Facility for Lower Mach Number P Swann, D Buttsworth, IH Jahn, R Frith, J Moran, A Webb, L Noller AIAA AVIATION FORUM AND ASCEND 2024, 4198, 2024 | 5 | 2024 |
| Commissioning of a Supersonic Nozzle Control Regulator in the TUSQ Facility P Swann, J Moran, D Buttsworth, IH Jahn AIAA SCITECH 2026 Forum, 1748, 2026 | | 2026 |
| Initial testing of a pilot storage heater for a supersonic wind tunnel A Webb, P Swann, D Buttsworth, I Jahn AIAC 2025: 21st Australian International Aerospace Congress, 173-178, 2025 | | 2025 |
| Commissioning of a supersonic test facility at UniSQ P Swann, J Moran, D Buttsworth 21st Australian International Aerospace Congress (AIAC21), 137-137, 2025 | | 2025 |
| Pressure recovery performance of a Mach 3 Ramjet inlet P Swann, J Moran, D Buttsworth AIAC 2025: 21st Australian International Aerospace Congress, 179-184, 2025 | | 2025 |
| Silencer for a blast nozzle MDC ROWLAND, TA SEEWALD, IJH JAHN, PB SWANN US Patent App. 18/039,598, 2024 | | 2024 |
| Thrust reduction system for a blast nozzle MDC ROWLAND, TA SEEWALD, IJH JAHN, PB SWANN US Patent App. 18/039,702, 2024 | | 2024 |
| Taylor-Couette-Poiseuille Flow Heat Transfer Experimental Data I Jahn, P Swann, H Russell The University of Queensland, 2020 | | 2020 |
