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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    Title :

    Tapered wing stalling


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Nazir, P.P. (author)

    Published in:

    Publication date :

    1935


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Stalling of tapered wings

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


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