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Browsing Aeronautical Research Council Reports & Memoranda by Author "J. L. Fulker"

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Aerodynamic Data for Three Supercritical Aerofoils, RAE(NPL)9515 AND 9530, AND RAE 9550. Parts I and II

J. L. Fulker (1975)

Part I compares the experimentally determined aerodynamic characteristics of two 10½% thick supercritical aerofoil sections, RAE(NPL)9515 and 9530, over the Mach number range 0.3 to 0.88 and angles of incidence from -0.82° ...

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