In the foregoing remarks I have made an attempt to touch on some of the structural problems met with in cantilever wings, and dealt rather fully with a certain type of single-spar construction. The experimental test wing was a first attempt to demonstrate the principles of this departure from orthodox methods. The result was a wing both torsionally stiff and of light weight - lighter than a corresponding biplane construction.


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    Titel :

    Cantilever Wings for Modern Aircraft: Some Aspects of Cantilever Wing Construction with Special Reference to Weight and Torsional Stiffness


    Beteiligte:
    Stieger, H J (Autor:in)

    Erscheinungsdatum :

    01.11.1929


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Cantilever wings for modern aircraft

    Stieger, H.J. | Engineering Index Backfile | 1929


    Cantilever wings for modern aircraft

    Stieger, H.J. | Engineering Index Backfile | 1929


    Cantilever wings for modern aircraft

    Stieger, H.J. | Engineering Index Backfile | 1929


    Cantilever Wings for Modern Aircraft

    Stieger, H.J. | Emerald Group Publishing | 1929