| Shock train unsteadiness characteristics, oblique-to-normal transition, and three-dimensional leading shock structure RL Hunt, M Gamba AIAA journal 56 (4), 1569-1587, 2018 | 62 | 2018 |
| On the origin and propagation of perturbations that cause shock train inherent unsteadiness RL Hunt, M Gamba Journal of Fluid Mechanics 861, 815-859, 2019 | 60 | 2019 |
| Response of a shock train to downstream back pressure forcing R Klomparens, JF Driscoll, M Gamba 54th AIAA aerospace sciences meeting, 0078, 2016 | 36 | 2016 |
| Relationship between intermittent separation and vortex structure in a three-dimensional shock/boundary-layer interaction RR Morajkar, RL Klomparens, WE Eagle, JF Driscoll, M Gamba, JA Benek AIAA Journal 54 (6), 1862-1880, 2016 | 31 | 2016 |
| Periodic forcing of a shock train in Mach 2.0 flow R Hunt, JF Driscoll, M Gamba 55th AIAA aerospace sciences meeting, 0088, 2017 | 23 | 2017 |
| Unsteadiness characteristics and three-dimensional leading shock structure of a Mach 2.0 shock train R Hunt, JF Driscoll, M Gamba 55th AIAA Aerospace Sciences Meeting, 0087, 2017 | 17 | 2017 |
| Fast approximations of spectral lineshapes to enable optimization of a filtered Rayleigh scattering experiment GJ Hunt, CR Ground, RL Hunt Measurement Science and Technology 31 (9), 095203, 2020 | 11 | 2020 |
| Scaling of pseudoshock length and pressure rise R Hunt, LM Edelman, M Gamba 2018 AIAA Aerospace Sciences Meeting, 1617, 2018 | 11 | 2018 |
| Boundary layer separation in a 3D shock train R Klomparens, M Gamba, JF Driscoll 53rd AIAA Aerospace Sciences Meeting, 1519, 2015 | 7 | 2015 |
| Flow Separation Associated with 3-D Shock-Boundary Layer Interaction (SBLI) RR Morajkar, RL Klomparens, WE Eagle, JF Driscoll, M Gamba 52nd Aerospace Sciences Meeting, 1138, 2014 | 7 | 2014 |
| Shock Train Structure and Dynamics R Hunt | 5 | 2018 |
| Locating the isolator shock-train leading edge with limited pressure information GJ Hunt, RL Hunt Journal of Propulsion and Power 37 (6), 876-892, 2021 | 4 | 2021 |
| Quantitative gas property measurements by filtered Rayleigh scattering: a review CR Ground, RL Hunt, GJ Hunt Measurement Science and Technology 34 (9), 092001, 2023 | 3 | 2023 |
| Application of flux-conserved modeling to an unsteady combustion driven pseudo-shock LM Edelman, M Gamba, R Hunt, A Auslender, JM Donbar, M Hagenmaier AIAA Scitech 2021 Forum, 1763, 2021 | 2 | 2021 |
| Three-dimensional structure and modeling of a normal bifurcated shock train from experimental measurements LM Edelman, M Gamba, R Hunt, A Auslender AIAA SCITECH 2022 Forum, 0370, 2022 | 1 | 2022 |
| Adaptive Pressure Profile Method to Locate the Isolator Shock Train Leading Edge Given Limited Pressure Information R Hunt, G Hunt AIAA Propulsion and Energy 2020 Forum, 3715, 2020 | 1 | 2020 |
| Using computational flow imaging to optimize filtered Rayleigh scattering measurements of an isolator shock train R Hunt, CR Ground, RA Baurle, P Danehy AIAA Propulsion and Energy 2019 Forum, 4016, 2019 | 1 | 2019 |
| Constrained Field Construction Using Bernstein Polynomial Derived Operators AH Auslender, RL Hunt, LM Edelman JANNAF Subcommittee Meetings, 2023 | | 2023 |
| Review of Surrogate Strategies and Regularization with Application to High-Speed Flows G Hunt, R Hunt, CD Marley The ITEA Journal of Test and Evaluation 44 (3), 2023 | | 2023 |
| Assessment of Pseudoshock Models Against Experiment in a Low-Aspect-Ratio Isolator LM Edelman, M Gamba, RL Hunt, A Auslender Journal of Propulsion and Power 39 (5), 653-664, 2023 | | 2023 |
