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Experiments in high-speed flows typically use wind tunnels with one of two nozzle geometries, which have generally been considered equivalent. We show that the nozzle geometry does in fact significantly affect the boundary-layers on the sidewalls and in the corners of the tunnel.

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This page is a summary of: Nozzle Geometry Effects on Corner Boundary Layers in Supersonic Wind Tunnels, AIAA Journal, August 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058310.
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