Model tested as high wing, midwing, and low wing monoplane; for each wing location tests were made with two amounts of dihedral and with partial span split flaps; results are presented and discussed.


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    Titel :

    Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. II. Rectangular, N.A.C.A. 23012 wing with circular fuselage and fin


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Bamber, M.J. (Autor:in) / House, R.O. (Autor:in)


    Erscheinungsdatum :

    1939


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :