1. Boundary Layer Transition (BOLT) Flight Experiment Overview
2. The effect of increased throat size on the nozzle-supply flow in reflected shock tunnels
3. Jacobs, P. A., Gollan, R. J., Potter, D. F., Zander, F., Gildfind, D. E., Blyton, P., Chan, W. Y. K., and Doherty, L. "Estimation of high-enthalpy flow conditions for simple shock and expansion processes using the ESTCj program and library," Mechanical Engineering Report 2011/02, School of Mechanical and Mining Engineering, The University of Queensland, Brisbane, Australia, 2014.
4. Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy