1. Experiments on Boundary-Layer Transition at Supersonic Speeds
2. Cooper, M., Mayo, Ed. E., and Julius, J. D., The Influence of Low Wall Temperature on Boundary Layer Transition and Local Heat Transfer on 2-Inch-Diameter Hemispheres at a Mach Number of 4.95 and a Reynolds Number Per Foot of 73.2 X W<> NASA TN D-391, July 1900.