Results of tests made in 1918 in old 4-ft. wind tunnel at Mass. Inst. of Technology, for purpose of securing data on effect of windshield form on total resistance of fuselage of good streamline shape.


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    Title :

    Wind tunnel tests of fuselages and windshields


    Additional title:

    U.S. Nat. Advisory Comm. Aeronautics -- Tech. Notes


    Contributors:


    Publication date :

    1925


    Size :

    6 pages


    Remarks:

    4 Figs. on supp. plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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