Tests made in Langley free flight tunnel at lift coefficient of 1.0, covered range of geometric dihedral angles from -- 20 to 20° and range of vertical tail areas from 0 to 15% of wing area; results compared with previously reported results of similar series of tests on conventional model having wing with aspect ratio of 6.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Lateral stability and control characteristics of free-flying model having unswept wing with aspect ratio of 2


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:


    Erscheinungsdatum :

    1948


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :