Tests on airship models in variable-density wind tunnel to determine drag coefficients at zero pitch, and effect of fins and cars and of flat and streamline protruberances located at various positions along hull; range of Reynolds Number from 1,300,000 to 33,000,000.


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    Title :

    Drag of two streamline bodies as affected by protuberances and appendages


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1932


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :