| Crossflow instability in a hypersonic boundary layer SA Craig, WS Saric Journal of Fluid Mechanics 808, 224-244, 2016 | 97 | 2016 |
| 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 |
| Hypersonic crossflow instability TS Kocian, AJ Moyes, HL Reed, SA Craig, WS Saric, SP Schneider, ... Journal of Spacecraft and Rockets 56 (2), 432-446, 2019 | 40 | 2019 |
| Experimental study of crossflow instability on a Mach 6 yawed cone SA Craig, WS Saric 45th AIAA Fluid Dynamics Conference, 2774, 2015 | 24 | 2015 |
| 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 |
| Crossflow instability on a yawed cone at Mach 6 SA Craig, WS Saric Procedia IUTAM 14, 15-25, 2015 | 14 | 2015 |
| Stability of high-speed, three-dimensional boundary layers SA Craig | 8 | 2015 |
| Fin-induced Shock Boundary Layer Interactions on a Flat Plate and Hollow Cylinder at Mach 5 JA Threadgill, L Jouannais, C Hader, J Flood, SA Craig, HF Fasel, ... AIAA SciTech 2022 Forum, 1816, 2022 | 7 | 2022 |
| Flow quality mapping of the Mach 4 quiet Ludwieg tube JT Flood, SA Craig, L Taubert AIAA Scitech 2020 Forum, 0360, 2020 | 5 | 2020 |
| Calibration and performance characterization of a Mach 5 Ludwieg tube KP Bearden, VE Padilla, L Taubert, SA Craig Review of Scientific Instruments 93 (8), 2022 | 3 | 2022 |
| Development of plasma-based controlled disturbances for the study of boundary layer transition and shock boundary layer interaction A Singh, JA Threadgill, JT Flood, SA Craig, JC Little, C Hader, HF Fasel AIAA Aviation 2021 Forum, 2822, 2021 | 3 | 2021 |
| Flow structure and heat transfer characterization of a blunt-fin-induced shock-wave/laminar boundary-layer interaction J Castro Maldonado, JA Threadgill, SA Craig, JC Little, SH Wernz AIAA Scitech 2021 Forum, 0748, 2021 | 2 | 2021 |
| First and Mack-mode instabilities in a flat-plate boundary layer at Mach 4 JT Flood, L Taubert, SA Craig AIAA Scitech 2020 Forum, 0361, 2020 | 2 | 2020 |
| Initial Flow Quality of the Mach 4 Quiet Ludwieg Tube JT Flood, L Taubert, SA Craig AIAA Aviation 2019 Forum, 3220, 2019 | 2 | 2019 |
| 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 |
| Calibration of a Mach 5 Ludwieg tube at the University of Arizona KP Bearden, VE Padilla, L Taubert, SA Craig AIAA AVIATION 2021 FORUM, 2950, 2021 | 1 | 2021 |
| 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 |
| Tip Sharpness Criterion for Hypersonic Wind-Tunnel Experiments SA Craig AIAA Journal 60 (12), 6947-6950, 2022 | | 2022 |
| Fin-Induced Shock Boundary Layer Interaction on Mach 5 cylinder. J Threadgill, SA Craig, J Little APS Division of Fluid Dynamics Meeting Abstracts, Q21. 008, 2021 | | 2021 |
| Dynamics of Richtmyer-Meshkov (RM) mixing with reshock S Mula, S Craig, K Prestridge APS Division of Fluid Dynamics Meeting Abstracts, M38. 002, 2016 | | 2016 |
Jerrod W. HofferthPostdoctoral Research Associate, Texas A&M UniversityVerified email at tamu.edu
