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Wind tunnel noise reduction at Mach 5 with a rod-wall sound shield. [for prevention of premature boundary layer transition on wind tunnel models]

T. R. Creel, I. E. Beckwith

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Key concepts: Wind tunnel, Shield, Boundary layer, Mach number, Supersonic wind tunnel, Noise (video), Sound (geography), Hypersonic wind tunnel

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Wind tunnel noise reduction at Mach 5 with a rod-wall sound shield. [for prevention of premature boundary layer transition on wind tunnel models] — Research Paper | ScholarLens