In the following we develop a non-autorotating monoplane wing. The conditions imposed on such a wing, aside from its freedom from autorotation,with respect to its polars and its construction, are taken into account as far as possible. It is indicated that the autorotation characteristics of a wing are dependent upon the speed of air flow as well as on the angle of yaw. This report postulates the knowledge of the behavior of certain conventional wings of different chords and cambers with respect to their air loads at large angles of attack.


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    Title :

    Development of a Non-autorotative Airplane Capable of Steep Landing


    Contributors:

    Publication date :

    1931-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



    Development of non-autorotative airplane capable of steep landing

    Schmidt, W. | Engineering Index Backfile | 1931


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    Schmidt, W. | Engineering Index Backfile | 1931



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