平特五不中

Aerodynamic

Members of laboratory:

Available flow facilities and major measurement techniques:

New 3 ft x 4 ft Low-Turbulence Subsonic Wind Tunnel
New 3 ft x 4 ft Low-Turbulence Subsonic Wind Tunnel (Rear View)

New 3 ft x 4 ft Low-Turbulence Subsonic Wind Tunnel
New 3 ft x 4 ft Low-Turbulence Subsonic Wind Tunnel (Rear View)

2 ft x 3 ft Subsonic Wind Tunnel

  • Three major subsonic wind tunnels
  • Thin-film sensor laboratory
  • Laser/optics flow measurement room
  • Particle image velocimetry technique
  • Laser Doppler Velocimetry technique
  • Hot-wire anemometry technique
  • Laser-induced fluorescence technique

Major equipment:

  • Q-swithched pulsed Nd:YAG lasers
  • CW Argon laser
  • He-Ne lasers
  • CCD camera and lenses
  • Multi-channel hot-wire anemometers
  • Computer-controlled traversing mechanisms

Laser/optics flow measurement equipment

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