Test Section

Closeup of test section

Velocity Field Using PIV

PIV Image of Uinf at time 1

Velocity Field Using PIV

PIV Image of Uinf at time 2

Effect of Microjet Control

Velocity Field with and without Control

Effect of Microjet Control

Noise Suppression using Microjets

Facilities

Supersonic Wind Tunnel

Supersonic Blowdown Wind Tunnel

  • Intermittent blow down style arrangement
  • A range of mach numbers can be run with the current design's ease of nozzle replacement
  • Test section is 66mm wide, 44mm high, and 305mm long, with the side walls and floor made from optical quality glass
  • The roof of the test section is removable for model mounting
  • Run times are up to 10 minutes at Mach 1.5 and 20 minutes at Mach 2
  • Operation is handled through a dedicated control room utilizing LabVIEW™ data acquisition program
  • A number of measurement techniques are available for research: Schlieren or Shadowgraph and Particle Image Velocimetry (PIV)