Fuselages were bodies of revolution with maximum diameters equal to 12% of fuselage length; nose shapes were circular, elliptical, and pointed; tests conducted for various angles of attack up to 30°; theoretical estimates of interference effect for zero angle of attack also included.


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    Title :

    Investigation of fuselage interference on pitot-static tube extending forward from nose of fuselage


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Letko, W. (author)


    Publication date :

    1947


    Size :

    21 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English