| 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 | 151 | 2016 |
| 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 | 115 | 2021 |
| Shock transition to detonation in channels with obstacles GB Goodwin, RW Houim, ES Oran Proceedings of the combustion institute 36 (2), 2717-2724, 2017 | 93 | 2017 |
| 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 | 41 | 2021 |
| Premixed flame stability and transition to detonation in a supersonic combustor GB Goodwin, ES Oran Combustion and Flame 197, 145-160, 2018 | 35 | 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 | 24 | 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 | 17 | 2021 |
| 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 | 13 | 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 | 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 | 11 | 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 |
| 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 | 9 | 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 |
| Analysis of Flame Structures in a Model Solid Fuel Ramjet Combustor with Increasing Reynold's Number RD DeBoskey, DA Kessler, TK Patel, BT Bojko, R Johnson, GB Goodwin, ... AIAA SCITECH 2024 Forum, 2595, 2024 | 5 | 2024 |
| 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 |
| Mean pressure gradient effects on the performance of ramjet cavity stabilized flames AJ Morales, DM Smerina, MR Thornton, CJ Rising, J Sosa, RF Johnson, ... Aerospace Science and Technology 141, 108533, 2023 | 4 | 2023 |
| The Influence of Chemical Reaction Models on Combustion Dynamics in an Opposed-Flow Solid Fuel Burner RD DeBoskey, DA Kessler, BT Bojko, RF Johnson, GB Goodwin AIAA SCITECH 2023 Forum, 0161, 2023 | 4 | 2023 |