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4-Foot Supersonic Unitary Plan Wind Tunnel

4-Foot Supersonic Unitary Plan Wind Tunnel

pgs. 2
National Aeronautics and Space Administration NASA’s Aeronautics Test Program 4-Foot Supersonic Unitary Plan Wind Tunnel  ... 
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Tags: Mach number, wind tunnel, Test Section, Langley Research Center, Reynolds number, supersonic wind tunnel, transonic tunnel, aerodynamic characteristics, NASA Aeronautics, Test Program
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8416054 5 views Language: English

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