| Effect of decreasing blockage ratio on DDT in small channels with obstacles GB Goodwin, RW Houim, ES Oran Combustion and Flame 173, 16-26, 2016 | 131 | 2016 |
| Shock transition to detonation in channels with obstacles GB Goodwin, RW Houim, ES Oran Proceedings of the combustion institute 36 (2), 2717-2724, 2017 | 81 | 2017 |
| Stabilized detonation for hypersonic propulsion DA Rosato, M Thornton, J Sosa, C Bachman, GB Goodwin, KA Ahmed Proceedings of the national academy of sciences 118 (20), e2102244118, 2021 | 80 | 2021 |
| Ignition criteria and the effect of boundary layers on wedge-stabilized oblique detonation waves CL Bachman, GB Goodwin Combustion and Flame 223, 271-283, 2021 | 32 | 2021 |
| Premixed flame stability and transition to detonation in a supersonic combustor GB Goodwin, ES Oran Combustion and Flame 197, 145-160, 2018 | 29 | 2018 |
| Mach five to ten morphing waverider: control point study AA Phoenix, RE Rogers, JR Maxwell, GB Goodwin Journal of Aircraft 56 (2), 493-504, 2019 | 17 | 2019 |
| Evaluation of droplet aerodynamic breakup models in supersonic and hypersonic flows A Hess, DA Kessler, RF Johnson, C Aguilera, J Sosa, GB Goodwin AIAA Scitech 2021 Forum, 0751, 2021 | 12 | 2021 |
| Numerical investigation of turbulent flame-vortex interaction in premixed cavity stabilized flames CJ Rising, GB Goodwin, RF Johnson, DA Kessler, J Sosa, M Thornton, ... Aerospace Science and Technology 129, 107805, 2022 | 9 | 2022 |
| Premixed ethylene-air combustion in a dual-mode scramjet cavity combustor with a turbulent inflow GB Goodwin, RF Johnson, D Kessler, HK Chelliah AIAA Propulsion and Energy 2019 Forum, 4270, 2019 | 9 | 2019 |
| Morphing high-temperature surfaces for shapeable hypersonic waverider vehicles AA Phoenix, JR Maxwell, GB Goodwin Smart Materials, Adaptive Structures and Intelligent Systems 58264, V002T03A012, 2017 | 9 | 2017 |
| Controlled detonation initiation in hypersonic flow J Sosa, DA Rosato, GB Goodwin, CL Bachman, ES Oran, KA Ahmed Proceedings of the Combustion Institute 38 (3), 3513-3520, 2021 | 8 | 2021 |
| Performance analysis of a hypersonic scramjet engine with a morphable waverider inlet GB Goodwin, JR Maxwell 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4651, 2017 | 8 | 2017 |
| Shapeable inlet manifold for hypersonic scramjet JR Maxwell, GB Goodwin 55th AIAA Aerospace Sciences Meeting, 1385, 2017 | 8 | 2017 |
| Flow Quality Numerical Characterization for Cold Adjustable Supersonic Wind Tunnel JR Maxwell, GB Goodwin 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 4318, 2017 | 7 | 2017 |
| Synthetic freestream turbulence generation at an inflow boundary condition GB Goodwin, CL Bachman, RF Johnson, DA Kessler AIAA Scitech 2021 Forum, 1846, 2021 | 5 | 2021 |
| Wedge-stabilized oblique detonation waves in a hypersonic hydrogen-air premixed freestream CL Bachman, GB Goodwin, K Ahmed AIAA Propulsion and Energy 2019 Forum, 4044, 2019 | 5 | 2019 |
| Discontinuous-Galerkin simulations of premixed ethylene-air combustion in a cavity combustor RF Johnson, GB Goodwin, AT Corrigan, A Kercher, HK Chelliah AIAA Scitech 2019 Forum, 1444, 2019 | 5 | 2019 |
| Numerical Modeling and performance analysis of a scramjet engine with a controllable waverider inlet design GB Goodwin, JR Maxwell US Patent App. 15/943,019, 2018 | 4 | 2018 |
| Characterization of Supersonic Wind Tunnel Flow Quality Using Planar Laser CO2 Rayleigh Scattering C Aguilera Munoz, J Sosa, EW Hyde, GB Goodwin, DA Kessler, AM Hess, ... AIAA Propulsion and Energy 2021 Forum, 3523, 2021 | 3 | 2021 |
| Large Eddy Simulation of Continuously Adjustable Hypersonic Wind Tunnel JR Maxwell, GB Goodwin 2018 Fluid Dynamics Conference, 3545, 2018 | 3 | 2018 |
