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December 31, 2015
- The powerful fan and motor at the heart of the Icing Research Tunnel is capable of producing continuous airspeeds up to 395 mph.
- PFM powered force model rotor
- Bell 609 Spinner Inlet Icing Model
- Technicians pose with the ERJ-170 airfoil set up for testing the IRT.
- Icing Research Tunnel (IRT) Data Acquisition
- Saturn Tour Dates: 2016
- Icing Research Tunnel (IRT) Quick Facts
- Icing Research Tunnel (IRT) Characteristics
- National Transonic Facility (NTF) Data Acquisition
- National Transonic Facility (NTF) Description