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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Bamber, M.J. (author) / House, R.O. (author)


    Publication date :

    1939


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :