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Bell 609 spinner inlet icing model. Technicians taking measurement of ice accretions after an icing test.
Technicians pose with the ERJ-170 airfoil set up for testing the IRT.
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F-18 tethered “free flight” model.
3% Blended Wing Body (BWB) – the “450” model in the 14 x 22 foot wind tunnel.
Isolated Rotor Test System in the 14 x 22 foot wind tunnel.
The Energy Efficient Transport (EET) Full Span model in the 14 x 22 foot wind tunnel.
The Energy Efficient Transport (EET) model tested in its semi-span configuration.
