A multiple manometer designed to integrate automatically the normal force over an airfoil section is described and its mathematical theory explained. The development of this instrument was conducted at the Langley Memorial Aeronautical Laboratory.


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    Title :

    An integrating manometer for use in wind tunnel pressure distribution measurements


    Contributors:

    Publication date :

    1931-05-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English