This report is on the changes in forces on each wing of a biplane cellule when either the stagger or the gap is varied. Since each test was carried up to a 90 degree angle of attack, the results may be used in the study of stalled flight and of spinning as well as in the structural design of biplane wings.


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    Titel :

    Wind Tunnel Pressure Distribution Tests on a Series of Biplane Wing Models


    Beteiligte:

    Erscheinungsdatum :

    01.07.1929


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Wind tunnel pressure distribution tests on series of biplane wing models

    Knight, M. / Noyes, R.W. | Engineering Index Backfile | 1929


    Wind tunnel pressure distribution tests on a series of biplane wing models

    Knight, Montgomery ;Noyes, Richard W. | SLUB | 1929


    Wind tunnel pressure distribution tests on a series of biplane wing models

    Knight, Montgomery ;Noyes, Richard W. | SLUB | 1929


    Wind tunnel pressure distribution tests on a series of biplane wing models

    Knight, Montgomery ;Noyes, Richard W. | SLUB | 1929