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