Stuart A. Craig

Journals/Publications

• Bearden, K. P., Padilla, V. E., Taubert, L., & Craig, S. A. (2022). Calibration and performance characterization of a Mach 5 Ludwieg tube. Review of Scientific Instruments, 93(8). doi:10.1063/5.0093052
• Craig, S. A. (2022). Tip sharpness criterion for hypersonic wind tunnel experiments. AIAA Journal, 60(12). doi:10.2514/1.J061853
• Craig, S. A., Kocian, T. S., Moyes, A. J., Reed, H. L., Saric, W. S., Schneider, S. P., & Edelman, J. B. (2019). Hypersonic Crossflow Instability. Journal of Spacecraft and Rockets, 56(2), 432-446. doi:10.2514/1.a34289
• Craig, S., Humber, R., Hofferth, J., & Saric, W. (2019). Nonlinear behaviour of the Mack mode in a hypersonic boundary layer. Journal of Fluid Mechanics, 872, 74-99. doi:10.1017/jfm.2019.359
• Kocian, T. S., Moyes, A. J., Reed, H. L., Craig, S. A., Saric, W. S., Schneider, S. P., & Edelman, J. B. (2018). Hypersonic Crossflow Instability. Journal of Spacecraft and Rockets. doi:10.2514/1.A34289
• Craig, S. A., & Saric, W. S. (2016). Crossflow instability in a hypersonic boundary layer. Journal of Fluid Mechanics, 808, 224--244. doi:10.1017/jfm.2016.643
• Craig, S. A., Prestridge, K., & Mula, S. M. (2016). Dynamics of Richtmyer-Meshkov (RM) mixing with reshock. Bulletin of the American Physical Society.
• Craig, S. A., & Saric, W. S. (2015). Crossflow Instability on a Yawed Cone at Mach 6. Procedia IUTAM. doi:10.1016/j.piutam.2015.03.019
• Craig, S. A., Prestridge, K., Wilson, B., & Mejia-Alvarez, R. (2015). Richtmyer-Meshkov mixing: experiments on the effect of initial conditions. Bulletin of the American Physical Society.
• Craig, S. A., & Saric, W. S. (2014). Experimental study of crossflow instability on a Mach 6 yawed cone. Bulletin of the American Physical Society.
• Craig, S. A., Saric, W. S., Hofferth, J. W., McClure, P. D., Vadyak, J., & Humble, R. A. (2013). Spatiotemporal structure of a millimetric annular dielectric barrier discharge plasma actuator. Physics of Fluids. doi:10.1063/1.4774334
• Craig, S. A., Saric, W. S., Hofferth, J. W., & Humble, R. A. (2011). Flow-field characterization of DBD plasma actuators as discrete roughness elements for laminar flow control. Bulletin of the American Physical Society.

Proceedings Publications

• Craig, S. A., Flood, J. T., Hader, C., & Fasel, H. F. (2023). Experimental measurements and numerical investigations of boundary-layer instabilities on a Mach 5 hollow cylinder. In AIAA SciTech 2023.
• Flood, J. T., Craig, S. A., Little, J., Fasel, H. F., Hader, C., Jouannais, L., & Threadgill, J. A. (2022). Fin-induced Shock Boundary Layer Interactions on a Flat Plate and Hollow Cylinder at Mach 5. In AIAA SciTech 2022.
• Little, J. C., Craig, S., Flood, J., Hader, C., Jouannais, L., Threadgill, J. A., Threadgill, J. A., Jouannais, L., Hader, C., Flood, J., Craig, S., & Little, J. C. (2022, January). Fin-induced Shock Boundary Layer Interactions on a Flat Plate and Hollow Cylinder at Mach 5. In AIAA SCITECH 2022 Forum, 21.
• Bearden, K. P., Taubert, L., Craig, S. A., & Padilla, V. (2021). Calibration of a Mach 5 Ludwieg tube at the University of Arizona. In AIAA Aviation 2021.
• Flood, J. T., Threadgill, J. A., Singh, A., Little, J. C., Hader, C., Fasel, H. F., & Craig, S. A. (2021). Development of Plasma-based Controlled Disturbances for the Study of Boundary Layer Transition and Shock Boundary Layer Interaction. In AIAA AVIATION 2021 FORUM.
• Maldonado, J. C., Craig, S. A., Little, J., Wernz, S., & Threadgill, J. A. (2021). Flow Structure and Heat Transfer Characterization of a Blunt-Fin-Induced Shock-Wave/Laminar Boundary-Layer Interaction. In AIAA SciTech 2021.
• Flood, J., Taubert, L., & Craig, S. (2020, January). First and Mack-mode instabilities in a flat-plate boundary layer at Mach 4. In AIAA SciTech 2020.
• Flood, J., Taubert, L., & Craig, S. (2020, January). Flow quality mapping of the Mach 4 Quiet Ludwieg Tube. In AIAA SciTech 2020.
• Taubert, L., Craig, S. A., & Flood, J. T. (2020). Correction: Flow quality mapping of the Mach 4 Quiet Ludwieg Tube. In AIAA SciTech 2020.
• Craig, S. A., Taubert, L., & Flood, J. T. (2019). Initial Flow Quality of the Mach 4 Quiet Ludwieg Tube. In AIAA Aviation 2019.
• Flood, J., Taubert, L., & Craig, S. (2019, June). Initial flow quality of the Mach 4 Quiet Ludwieg Tube. In AIAA Aviation 2019.
• Craig, S. A., Edelman, J. B., Schneider, S. P., Saric, W. S., Reed, H. L., Moyes, A., & Kocian, T. S. (2018). Hypersonic Crossflow Instability. In AIAA SciTech 2018.
• Craig, S. A., & Saric, W. S. (2015). Experimental study of crossflow instability on a Mach 6 yawed cone. In AIAA Aviation 2015.
• Craig, S. A., Saric, W. S., & Humble, R. A. (2011). Characterization of the Flowfield Structure of an Annular Dielectric Barrier Discharge Plasma Actuator. In 41st AIAA Fluid Dynamics Conference.

Poster Presentations

• Tronstad, L., Threadgill, J. A., Little, J. C., & Craig, S. A. (2023). Heat Flux Measurements and Transition Prediction for the Construction of Surrogate Aerodynamic Databases. UCAH Spring Forum.

Presentations

• Craig, S. (2017, Apr 17). High-speed stability and transition experiments at the University of Arizona. Invited Seminar. New Mexico State University.
• Craig, S. (2017, Feb 17). Boundary-layer stability and transition experiments at the University of Arizona. Invited Seminar. Purdue University.
• Craig, S. (2017, Mar 17). High-speed stability and transition experiments at the University of Arizona. Invited Seminar. NASA Langley Research Center.
• Mula, S., Craig, S., & Prestridge, K. (2016, 11). Dynamics of Richtmyer-Meshkov (RM) mixing with reshock. APS Division of Fluid Dynamics 2016. Portland, OR: American Physical Society.