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  1. Instability and Transition on the ROTEX-T Cone-Flare in Supersonic Quiet Flow
  2. Effect of Surface Deformation on Hypersonic Transitional Shock-Wave/Boundary-Layer Interactions on the ROTEX-T Cone-Flare
  3. Effect of Model Size in the AFOSR--Notre Dame Large Mach-6 Quiet Tunnel
  4. Nosetip Bluntness Effects on the ROTEX-T Cone-Flare
  5. Unsteady Characteristics and Enhanced Determination of Reattachment for Hypersonic Transitional Shock-Wave/Boundary-Layer Interactions
  6. Preliminary Measurements on the BOLT Geometry in the Supersonic Low Disturbance Tunnel
  7. Separation and Transition on the ROTEX-T Cone-Flare