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    Title :

    Aerodynamic Heating of a Thin, Unswept, Untapered, Multiweb, Aluminum-alloy Wing at Mach Numbers up to 2.67 as Determined from a Free-flight Investigation of a Rocket-propelled Model


    Contributors:

    Publication date :

    1957-08-06


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English