Windkanaluntersuchungen an dunnen superkritischen Profilen im hohen Unterschall

Technical Report

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(GEN) The aerodynamic performance of three supercritical aerofoils for Mach number of 0.6 to 0.95 was compared with that of a NACA 64a(1.33)05 aerofoil. All aerofoils were 5 per cent thick
(DAT) 1982

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