| 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 |
| 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 Ablation on Boundary Layer Stability of the Reentry F Flight Vehicle RE Rogers, OM Schroeder, LJ Melander, GV Candler AIAA AVIATION 2022 Forum, 3775, 2022 | 3 | 2022 |
| Mach 5–3.5 morphing waverider accuracy and aerodynamic performance evaluation AA Phoenix, JR Maxwell, RE Rogers Journal of Aircraft 56 (5), 2047-2061, 2019 | 2 | 2019 |
| Investigation of Boundary Layer Stability Using the Parabolic Stability Equations on a Coupled Simulation of the Reentry F Flight Experiment RE Rogers University of Minnesota, 2022 | | 2022 |
Jesse MaxwellUS Naval Research LaboratoryPotvrđena adresa e-pošte na nrl.navy.mil
