Supersonic pressure distributions for tip and trailing edge controls on 60 deg delta wing


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    Title :

    Analysis of pressure distributions for a series of tip and trailing-edge controls on a 60 deg wing at Mach numbers of 1.61 and 2.01


    Contributors:

    Publication date :

    1958-05-16


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English