| High-bandwidth optical measurements of the second-mode instability in a Mach 6 quiet tunnel J Hofferth, R Humble, D Floryan, W Saric 51st AIAA aerospace sciences meeting including the new horizons forum and …, 2013 | 62 | 2013 |
| Boundary-layer instability and transition on a flared cone in a Mach 6 quiet wind tunnel J Hofferth, W Saric, J Kuehl, E Perez, T Kocian, H Reed International Journal of Engineering Systems Modelling and Simulation 47 5 …, 2013 | 53 | 2013 |
| Nonlinear behaviour of the Mack mode in a hypersonic boundary layer SA Craig, RA Humble, JW Hofferth, WS Saric Journal of Fluid Mechanics 872, 74-99, 2019 | 52 | 2019 |
| The Mach 6 quiet tunnel at Texas A&M: quiet flow performance J Hofferth, R Bowersox, W Saric 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 4794, 2010 | 52 | 2010 |
| Boundary-layer transition on a flared cone in the Texas A&M Mach 6 quiet tunnel J Hofferth, W Saric 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2012 | 28 | 2012 |
| Supersonic freestream density fluctuations from focused laser differential interferometry and pitot-probe measurements JM Lawson, MC Neet, JW Hofferth, JM Austin AIAA journal 60 (9), 5173-5186, 2022 | 26 | 2022 |
| Repetitively pulsed hypersonic flow apparatus for diagnostic development R Sánchez-González, R Srinivasan, J Hofferth, DY Kim, AJ Tindall, ... AIAA journal 50 (3), 691-697, 2012 | 26 | 2012 |
| Aerodynamic response to a compliant panel in mach 4 flow SJ Peltier, BE Rice, J Szmodis, DR Ogg, JW Hofferth, ME Sellers, ... AIAA Aviation 2019 forum, 3541, 2019 | 25 | 2019 |
| Spatiotemporal structure of a millimetric annular dielectric barrier discharge plasma actuator RA Humble, SA Craig, J Vadyak, PD McClure, JW Hofferth, WS Saric Physics of Fluids 25 (1), 2013 | 22 | 2013 |
| Freestream effects on boundary layer disturbances for HIFiRE-5 MP Borg, RL Kimmel, JW Hofferth, RD Bowersox, CL Mai 53rd AIAA Aerospace Sciences Meeting, 0278, 2015 | 19 | 2015 |
| Investigation of secondary motion in high speed flow BE Rice, NJ Bisek, S Peltier, JW Hofferth 55th AIAA Aerospace Sciences Meeting, 0526, 2017 | 12 | 2017 |
| Design, assembly, and calibration of a focusing schlieren system D Floryan, J Hofferth, W Saric no. Fig 2, 1-11, 2012 | 12 | 2012 |
| Reactivation of VKF Wind Tunnel D by AFRL at AEDC: Supersonic Performance and Freestream Characterizations JW Hofferth, DR Ogg AIAA Aviation 2019 Forum, 2856, 2019 | 11 | 2019 |
| Reactivation of VKF Wind Tunnel D by AFRL at AEDC: Overview and Subsystem Checkout Results JW Hofferth, DR Ogg 22nd AIAA International Space Planes and Hypersonics Systems and …, 2018 | 11 | 2018 |
| Structure of secondary motion in a Mach 2 boundary layer SJ Peltier, BE Rice, NJ Bisek, CK McKenna, JW Hofferth 2018 AIAA Aerospace Sciences Meeting, 0583, 2018 | 11 | 2018 |
| Reynolds number effects on secondary motion in corner flow boundary layers CK McKenna, BE Rice, NJ Bisek, SJ Peltier, JW Hofferth AIAA Aviation 2019 Forum, 3342, 2019 | 9 | 2019 |
| Mach Number Effects on Secondary Motion in Corner Flow Boundary Layers CK McKenna, BE Rice, NJ Bisek, SJ Peltier, JW Hofferth AIAA Scitech 2020 Forum, 0835, 2020 | 3 | 2020 |
| Characterization of the Flowfield Structure of an Annular Dielectric Barrier Discharge Plasma Actuator S Craig, R Humble, J Hofferth, W Saric 41st AIAA Fluid Dynamics Conference and Exhibit, 3987, 2011 | 2 | 2011 |
| Flow-field characterization of DBD plasma actuators as discrete roughness elements for laminar flow control SA Craig, RA Humble, JW Hofferth, WS Saric APS Division of Fluid Dynamics Meeting Abstracts 64, M23. 005, 2011 | 1 | 2011 |
| Boundary-layer transition on a flared cone in a Mach 6 quiet wind tunnel J Hofferth, W Saric APS Division of Fluid Dynamics Meeting Abstracts 63, CE. 004, 2010 | 1 | 2010 |
