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Design and preliminary test results at Mach 5 of an axisymmetric slotted sound shield. [for supersonic wind tunnels (noise reduction in wind tunnel nozzles)

I. E. Beckwith, A. J. Spokowski, W. D. Harvey, P. C. Stainback

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Key concepts: Supersonic wind tunnel, Supersonic speed, Mach number, Wind tunnel, Hypersonic wind tunnel, Shield, Acoustics, Noise (video)

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Design and preliminary test results at Mach 5 of an axisymmetric slotted sound shield. [for supersonic wind tunnels (noise reduction in wind tunnel nozzles) — Research Paper | ScholarLens