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  1. Shock Impingement Interaction on a One Degree-of-Freedom Slender Hypersonic Vehicle in Mach 5 Flow
  2. Pressure field and mean deflection estimation of a hypersonic vehicle model in Mach 5 flow
  3. Experimental Study on the Effect of Shock Strength and Mach Number on the Unsteadiness of Ramp-Induced Shock/Boundary-Layer Interaction Using Fast-Response PSP
  4. Effect of wall thickness of missiles and rockets on the vibrations experienced during flight
  5. Unsteadiness in Shock/Boundary-Layer Interaction Over a Compliant Panel at Mach 2
  6. Low order analysis of panel vibration under ramp-induced shock / boundary layer interaction
  7. Experimental test of skin panel vibrations for supersonic vehicles