A. K. Sreekanth

• Aerodynamic predictive methods and their validation in hypersonic flows
• Drag measurements of circular cylinders and spheres in the transition regime at a Mach number of 2
• Drag measurements on circular cylinders and spheres in the transition regime at a Mach number of 2
• Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel