Report presents the results of tests conducted on 28 wing-fuselage combinations made in the variable-density wind tunnel as a part of the wing-fuselage interference program being conducted therein and in addition to the 209 combinations previously reported in NACA-TR-540. These tests practically complete the study of combinations with a rectangular fuselage and continue the study of combinations with a round fuselage and a tapered wing.


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    Titel :

    Interference of Wing and Fuselage from Tests of 28 Combinations in the NACA Variable-Density Tunnel


    Beteiligte:

    Erscheinungsdatum :

    01.01.1937


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch