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Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

Title:Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
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Note:National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985
  
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Subject:Aerodynamics, Transonic
Subject:Aerofoils -- Testing -- Statistics
Subject:Low temperature research
Subject:Reynolds number
Subject:Transonic wind tunnels
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