Boundary Layer and Subsonic Wind Tunnel (BLAST)

The Boundary Layer and Subsonic Tunnel (BLAST) is a closed-return wind tunnel facility consisting of two test sections: one for reproducing high Reynolds-number boundary layer flows, and a second test section for subsonic aeronautical applications. The dual test-section wind tunnel enables tests for a wide range of applications, such as boundary-layer flows, transport phenomena, wind engineering, wind energy, urban flows, aerodynamics, aeronautics, aeroelasticity, and sport aerodynamics. Full optical access to the test sections and state-of-the art instrumentation are available for highly accurate experiments.

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