Affiliation:
1. Arizona State University
2. Cranfield University
Publisher
American Institute of Aeronautics and Astronautics
Reference21 articles.
1. Burbank, P. B., Collins, I. K., and Newlander, R. A. “Heat-transfer and pressure measurements on a flat-plate surface and heat-transfer measurements on attached protuberances in a supersonic turbulent boundary layer at Mach numbers of 2.65, 3.51, and 4.44,” 1962.
2. Protuberance interference heating in high-speed flow
3. Measurement of shock wave unsteadiness using a high-speed schlieren system and digital image processing
4. Hypersonic interference heating in the vicinity of surface protuberances