Results of tests carried out at speed of 42 ft per sec in 2-ft wind tunnel in Aeronautical Department of Queen Mary College; maximum chore of airfoils was 2.8 in; percentage of stall at various incidences, for three different wings; burbling disturbance along span of two wings; pigeon wing.


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    Titel :

    Tapered wing stalling


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:
    Nazir, P.P. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1935


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Stalling of tapered wings

    Lachmann, G.V. | Engineering Index Backfile | 1936


    Stalling of tapered wings

    Smith, R.H. | Engineering Index Backfile | 1936


    Stalling of tapered wings

    Nazir, P.P. | Engineering Index Backfile | 1935


    The Stalling of Tapered Wings

    Emerald Group Publishing | 1937


    On stalling of highly tapered wings

    Millikan, C.B. | Engineering Index Backfile | 1936