Aerodynamics Laboratory |
- TFI Cobra Probe
- Pitot-static tube and data acquisition system
- Force balance (lift, drag, and pitch)
- Subsonic closed return wind tunnel (1.12m by 0.71 m by 0.53 m test section, <30 m/s)
- Subsonic open return wind tunnel (xm by xm by x m test section, <20 m/s)
- Subsonic open return wind tunnel (xm by xm by x m test section, <3 m/s)
- Wind tunnel planar traversing probe
- 20 channel handheld voltage and thermocouple datalogger
- 40 channel data acquisition system, including thermocuples and thermistors
- Cold plate and recirculating chiller
- Refrigerant charging station
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