Methods of maintaining lateral stability with particular regard to latest type of Handley Page slot; problems of longitudinal control beyond stall; suggestions to produce fully controllable spin-proof airplane capable of being landed in restricted areas; calculation of distribution of lift and induced velocity for airfoil partly stalled. (See also - discussion p 319-38)


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    Titel :

    Control beyond stall


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:
    Lachmann, G.V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1932


    Format / Umfang :

    44 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Thurston wing-tip rotors: control beyond stall

    Thurston, A.P. / Hartshorn, A.S. | Engineering Index Backfile | 1934


    Thurston wing-tip rotors: Control beyond stall

    Thurston, A.P. | Engineering Index Backfile | 1934


    The longitudinal control of an aeroplane beyond the stall

    Garner, H. M. ;Wright, K. V. | SLUB | 1929


    The longitudinal control of an aeroplane beyond the stall

    Garner, H. M. / Wright, K. V. | TIBKAT | 1929