| Numerical tool for quantifying energy deposition effects on representative hypersonic vehicle structures JH Moran, BR Capra, AJ Neely Aerospace Science and Technology 116, 106862, 2021 | 13 | 2021 |
| Effects of Aerothermal Shape Distortion on Hypersonic Vehicle Performance in Cruise L Pollock, J Moran, AJ Neely 25th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2023 | 7 | 2023 |
| Wind-Tunnel based Free-Flight Testing of a Viscous Optimised Hypersonic Waverider JH Moran, LP McQuellin, L Pollock, AJ Neely, D Munk, F Zander AIAA SciTech 2023 Forum, 1385, 2023 | 5 | 2023 |
| Joule heated hot wall models in hypersonic wind tunnel facilities for energy deposition studies JH Moran, BR Capra, LP McQuellin Aerospace Science and Technology 126, 107627, 2022 | 3 | 2022 |
| Aerothermal Analysis of 3D Concave Cone in Hypersonic Flow in SCIROCCO B Capra, J Moran, M Brown, R Boyce, E Trifoni, A Schettino, C Purpura, ... Proc. of the 32nd International Symposium on Shock Waves (ISSW32), 2019 | 3 | 2019 |
| Numerical and Experimental Techniques for Quantifying Energy Deposition Effects on Representative Hypersonic Vehicle Structures JH Moran MS Thesis, Univ. of New South Wales Canberra, Canberra, ACT, Australia, 2021 | 2 | 2021 |
| Mach 6 and Mach 7 Conditions in TUSQ at Reynolds Numbers up to 30 Million J Moran, DR Buttsworth, L Noller AIAA AVIATION FORUM AND ASCEND 2024, 4197, 2024 | 1 | 2024 |
| A Numerical Analysis of Energy Deposition into a Hot Wall under Hypersonic Conditions JH Moran, BR Capra, A Neely 23rd AIAA International Space Planes and Hypersonic Systems and Technologies …, 2020 | 1 | 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 | | 2024 |
