1. L.H. Wilbur, Re-entry Aerodynamics, AIAA Education Series, Washington, 1988.
2. Hypersonic convective heat transfer over 140° blunt cones in different gases;Stewart;AIAA J. Spacecrafts Rockets,1994
3. Fore body convective hypersonic heat transfer measurements over large angle blunt cones;Jagadeesh;AIAA J. Spacecrafts Rockets,2000
4. N. Sahoo, Simultaneous measurement of aerodynamic forces and convective surface heat transfer rates for large angle blunt cones in hypersonic shock tunnel, Ph.D. Dissertation, Department of Aerospace Engineering, Indian Institute of Science, Bangalore, India, July 2003.
5. Reduction of data from thin-film heat-transfer gauge: a concise numerical technique;Cook;AIAA J.,1966