The FSU Anechoic Wind Tunnel is an open-circuit subsonic facility which has a 36" x 48" x 120" test section with a speed range of approximately 18-75 m/s. The facility employs a 450-hp centrifugal fan and has an anechoic chamber with a 250 Hz cut-on frequency enclosing the test section. The open-jet can be converted into a closed-wall wind tunnel as it has a removable test section with excellent optical access. The facility will be used for aerodynamic and aeroacoustic studies of various flow-induced noise phenomenon and boasts state-of-the-art experimental fluid dynamic and aeroacoustic measurement capabilities.
Item | Specification |
---|---|
Wind Tunnel | Open-circuit, open-jet or dosed walled |
Test Section | 48" X 36" X 120" |
Mach Number Range | 0.05-0.22 |
Anechoic Chamber Low Frequency Cutoff | 250 Hz |
Background Noise* | 80 dBA (M=0.15) |
Turbulence Intensity | <0.1% |
RMS Inlet Flow Nonuniformity | <1% |
*Currently not fully treated