Title: Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Subjects: Aerodynamics, Transonic, Aerofoils, Airfoil profiles, Boeing aircraft, Cryogenic wind tunnels, High Reynolds number, Pressure distribution, Reynolds number, Statistics, Supercritical airfoils, Testing, Transonic Aerodynamics, Two dimensional bodies, Wind tunnel models, Wind tunnel tests